command: 
 ./cs_solver --param RANS-2D-1.xml

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

                                  (R)
                      Code_Saturne

                      Version 4.0.2


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

  revision 4.0.2
  build jue 18 feb 2016 17:57:20 ART
  MPI version 2.1 (Open MPI 1.6.2)


  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:                mar 31 may 2016 15:03:18 ART
  System:              Linux 2.6.32-431.11.2.el6.x86_64
  Machine:             seshat.santafe-conicet.gov.ar
  Processor:           model name	: Intel(R) Xeon(R) CPU E5-2640 v2 @ 2.00GHz
  Memory:              96774 MB
  User:                lgarelli ()
  Directory:           /home/lgarelli/Runs/Cavitation/Case_2/RESU/20160531-1503
  OpenMP threads:      6
  Processors/node:     16
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

  External libraries for partitioning:
    ParMETIS 4.0.3
    SCOTCH 5.1.10

 Reading metadata from file: "mesh_input/mesh_01"
 Reading metadata from file: "mesh_input/mesh_02"
 Reading metadata from file: "mesh_input/mesh_03"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              8 (Nb variables                )
       NSCAL  =              1 (Nb scalars                  )
       NSCAUS =              1 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              8 (Nb cell properties          )


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.10000E+04 (Reference density           )
       VISCL0 =    0.10000E-02 (Ref. molecular dyn. visc.   )
       CP0    =    0.41820E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.00000E+00 (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        )

  -- Liquid phase:
       ROL    =    0.10000E+04 (Reference density           )
       MUL    =    0.10000E-02 (Ref. molecular dyn. visc.   )

  -- Gas phase:
       ROV    =    0.10000E+01 (Reference density           )
       MUV    =    0.10000E-04 (Ref. molecular dyn. visc.   )

  -- Vaporization/condensation model (Merkle)
       PRESAT =    0.20000E+04 (Saturation pressure         )
       LINF   =    0.10000E+00 (Reference length scale      )
       UINF   =    0.63000E+01 (Reference velocity          )

  -- Eddy-viscosity correction (Reboud correction)
       ICVEVM =              1 (Activated (1) or not (0)    )
       MCAV   =    0.10000E+02 (mcav constant               )


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


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

   - Commons
       ITHERM =              0 (0: no thermal model         )
                               (1: temperature              )
                               (2: enthalpy                 )
                               (3: total energy             )
       ITPSCL =              0 (0: none                     )
                               (1: temperature in Kelvin    )
                               (2: temperature in Celsius   )
       ISCALT =             -1 (Thermal scalar number       )


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

 --- Continuous phase:

   - Commons
       ITURB  =             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   =    0.63000E+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 =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.50000E-06 (Minimum time step           )
       DTMAX  =    0.50000E-02 (Maximum time step           )
       DTREF  =    0.50000E-05 (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
 Void Fraction         1  0.1000E+01
 k                     1  0.1000E+01
 omega                 1  0.1000E+01
 scalar1               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
 Void Fraction         1      0      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
 scalar1               1      1      1      1      0 0.10E+01 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
 Void Fraction       100      1  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
 scalar1             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
 Void Fraction         1     -1  0.1500E+01
 k                     1     -1  0.1500E+01
 omega                 1     -1  0.1500E+01
 scalar1               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               )
       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              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
 Void Fraction     0.1000E-07      1
 k                 0.1000E-07      1
 omega             0.1000E-07      1
 scalar1           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    )


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


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

-------------------------------------------------------------
 Variable         Number ISCACP ITURT      VISLS0      SIGMAS
-------------------------------------------------------------
 scalar1               1      0      0  0.1830E-01  0.1000E+01
---------------------------------------------------------------------

------------------------------------
 Variable         Number      RVARFL
------------------------------------
 scalar1               1  0.8000E+00
-------------------------------------------

-------------------------------------------------------
 Variable         Number ICLVFL      SCAMIN      SCAMAX
-------------------------------------------------------
 scalar1               1     -1 -0.1000E+13  0.1000E+13
-------------------------------------------------------

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

       For each scalar, the number indicates it's rank
         in the list of all scalars. User scalars are placed
         first, from 1 to NSCAUS. Specific physics scalars
         are placed at the end, from
         NSCAUS+1 to NSCAPP+NSCAUS=NSCAL.

       ISCACP = 0 or 1     2   (use Cp or not               )
       VISLS0 = >0             (Reference viscosity         )
       SIGMAS = >0             (Schmidt                     )
       RVARFL = >0             (Rf, cf variance dissipation )
       ICLVFL = 0, 1 or 2      (Variance clipping mode      )
       SCAMIN =                (Min authorized value        )
       SCAMAX =                (Max authorized value        )
        For variances, SCAMIN is ignored and SCAMAX is used
          only if ICLVFL = 2

------------------------------------------------------
   Scalar        THETSS    IVSEXT      THETVS
------------------------------------------------------
          1  0.0000E+00         0  0.0000E+00
------------------------------------------------------

       THETSS =                (theta for source terms      )
                               ((1+theta).new-theta.old     )
       IVSEXT =                (extrap. total viscosity     )
                               (0: explicit                 )
                               (1: n+thetvs with thetvs=1/2 )
                               (2: n+thetvs with thetvs=1   )
       THETVS =                (theta for scalar diffusivity
                               ((1+theta).new-theta.old     )


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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =           5000 (Final time step required    )

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


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


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

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

 --- Post-processed variables


Velocity
Pressure
Void Fraction
k
omega
scalar1
TurbVisc
CourantNb
FourierNb
total_pressure
Density Old
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              4 (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 Void Fraction                 -1
         7 k                             -1
         8 omega                         -1
         9 scalar1                       -1
        11 LamVisc                       -1
        12 TurbVisc                      -1
        13 CourantNb                     -1
        14 FourierNb                     -1
        15 total_pressure                -1
        16 Density Old                   -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 Void Fraction                  0
         7 k                              0
         8 omega                          0
         9 scalar1                        0
        12 TurbVisc                    -999
        13 CourantNb                   -999
        14 FourierNb                   -999
        15 total_pressure              -999
        16 Density Old                 -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              0 (Force exerted by the
                                     fluid on the boundary)
       ipstft =              1 (Thermal flux   at boundary)
       ipsttb =              0 (Temperature    at boundary)
       ipstnu =              0 (Dimensionless thermal
                                          flux at boundary)


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


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

       IALE   =              0 (1: activated                )
       NALINF =              0 (Fluid initialization
                                                  iterations)
       IFLXMW =              0 (ALE mass flux computation
                                0: thanks to vertices
                                1: thanks to mesh velocity)


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


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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.8
      options: 
      time dependency: fixed mesh
      output: every 5 time steps and at calculation end


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

 Reading file:        mesh_input/mesh_02
 Finished reading:    mesh_input/mesh_02

 Reading file:        mesh_input/mesh_03
 Finished reading:    mesh_input/mesh_03


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

  Selection criteria: "join3 or join4"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.10000
    Maximum angle between joined face planes: 25.00000

  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:          57000
     Number of interior faces: 113130
     Number of boundary faces: 115740
     Number of vertices:       115746

  Global number of boundary faces selected for joining:        200

  Element selection successfully done.
  Determination of possible face intersections:

    bounding-box tree layout: 1D

  Global number of intersections detected:         1807
    Vertex-Vertex intersections:            1807
    Other intersections:                       0

  Joining operation is conforming.

  Edge intersections and vertex creation done.

  Pre-merge for 202 global element couples.

  No need to merge 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.

  Global number of faces after splitting:        100

  Global configuration after the joining operation:
     Global number of border faces to add:          0

  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:          57000
     Number of interior faces: 113230
     Number of boundary faces: 115540
     Number of vertices:       115544


  Joining  1 completed (0.107 s).

 -------------------------------------------------------
  Joining number 2:

  Selection criteria: "join5 or join6"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.10000
    Maximum angle between joined face planes: 25.00000

  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:          57000
     Number of interior faces: 113230
     Number of boundary faces: 115540
     Number of vertices:       115544

  Global number of boundary faces selected for joining:        200

  Element selection successfully done.
  Determination of possible face intersections:

    bounding-box tree layout: 2D

  Global number of intersections detected:         1808
    Vertex-Vertex intersections:            1808
    Other intersections:                       0

  Joining operation is conforming.

  Edge intersections and vertex creation done.

  Pre-merge for 202 global element couples.

  No need to merge 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.

  Global number of faces after splitting:        100

  Global configuration after the joining operation:
     Global number of border faces to add:          0

  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:          57000
     Number of interior faces: 113330
     Number of boundary faces: 115340
     Number of vertices:       115342


  Joining  2 completed (0.104 s).

  All joining operations successfully finished:

    Wall clock time:                 0.213

 Number of cells:                                      57000

 ----------------------------------------------------------
 Number of cells + halo cells:                         57000


 ----------------------------------------------------------
 Number of interior faces:                             113330

 ----------------------------------------------------------
 Number of boundary faces:                             115340

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =          4
      2 : [          3 ;          4 ] =      56996

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

 Writing file:        mesh_output
 Finished writing:    mesh_output
 Number of cells:                                      57000

 ----------------------------------------------------------
 Number of cells + halo cells:                         57000


 ----------------------------------------------------------
 Number of interior faces:                             113330

 ----------------------------------------------------------
 Number of boundary faces:                             115340

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =          4
      2 : [          3 ;          4 ] =      56996

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

 Renumbering mesh:

   renumbering for cells:
     pre-numbering:                       none
     cells adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for interior faces:
     cell adjacency pre-ordering:         lowest id first
     faces adjacent to ghost cells last:  no
     numbering:                           multipass

   renumbering for boundary faces:
     numbering:                           none

 Number of thread pools for interior faces :          6
 Number of threading groups for interior faces :      3
 Estimated thread imbalance for interior faces :      2.94715e-03

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

 Matrix bandwidth for volume mesh :          36880
 Matrix profile/lines for volume mesh :      355

 Mesh coordinates:               minimum    and maximum
                       X : -1.1000000e-02  9.0680000e-02
                       Y : -9.8685533e-03  5.0003000e-03
                       Z : -2.5451939e-18  5.0000000e-06
 Mesh
     Number of cells:          57000
     Number of interior faces: 113330
     Number of boundary faces: 115340
     Number of vertices:       115342

 Groups:
    "Symmetry12"
       boundary faces:        34000
    "Symmetry3"
       boundary faces:        40000
    "Symmetry45"
       boundary faces:        40000
    "conv"
       boundary faces:          120
    "div"
       boundary faces:          200
    "div2"
       boundary faces:          100
    "entree"
       boundary faces:          100
    "fluid"
       cells:                 57000
    "join3"
       interior faces:          100
    "join4"
       interior faces:          100
    "join5"
       interior faces:          100
    "join6"
       interior faces:          100
    "sortie"
       boundary faces:          100
    "wall12"
       boundary faces:          220
    "wall3"
       boundary faces:          200
    "wall4"
       boundary faces:          300

 --- Information on the volumes
       Minimum control volume      =  4.2944887e-16
       Maximum control volume      =  4.1513359e-12
       Total volume for the domain =  3.8388330e-09

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

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

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

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

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

 Computing geometric quantities (0.126 s)
                                                             
       ALMAX  =    0.15759E-02 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  Void Fraction     0.1000E-09  0.1000E-09
  k                 0.2381E-01  0.2381E-01
  omega             0.9792E+02  0.9792E+02
  scalar1           0.0000E+00  0.0000E+00
 ---------------------------------

                dt  0.5000E-05  0.5000E-05
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.500000000E-05   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1000E+04  0.1000E+04
  molecular_viscos  0.1000E-02  0.1000E-02
  turbulent_viscos  0.2432E+00  0.2432E+00
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 scalar1               1  0.1830E-01  0.1830E-01
 -----------------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         100
Smooth wall               5        1140
Rough wall                6           0
Symmetry                  4      114000
Free outlet               3         100
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with pressure Dirichlet condition detected
Update of reference point for total pressure
 XYZP0 =    0.90680E-01   0.64258E-05   0.25000E-05



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100         0.000000000E+00
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.15178E-01 0.18677E-01
   Dimensionless distance   yplus :  0.35460E-01 0.66650E-01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1140
   Total number of wall faces                   :       1140
------------------------------------------------------------


                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.23578E-05 Max distance =    0.49568E-02
                                                             
     (Distance calculation done in       1224 iterations)


@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.64891E-12
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1264E-03


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45583E-03     565   0.73675E-03   0.12285E+07 0.20000E+06 
c  Velocity[X]                                      0.12175E+07 
c  Velocity[Y]                                      0.10951E+05 
c  Velocity[Z]                                      0.15880E+00 
c  Pressure     0.21346E-07    3153   0.14001E+00   0.10068E+01 0.20000E+06 
c  Void Fractio 0.11895E-08      28   0.48641E-08   0.00000E+00 0.00000E+00 
c  k            0.29657E-03     262   0.35151E-03   0.48019E+00 0.13098E+05 
c  omega        0.51342E+07     429   0.13673E-02   0.17868E+24 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction     -0.00076205                         57000
a  k            
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.52522           11.28          5.1724          1.8288
v  Velocity[Y]            -1.0741          2.7543       -0.047866        -0.10162
v  Velocity[Z]           -0.30744         0.39466     -1.5089e-06     -4.8812e-08
v  ǁVelocityǁ             0.52847          11.327          5.2036          1.8371
v  Pressure             1.467e+05      4.8545e+07       2.956e+07      1.0385e+07
v  Void Fraction            1e-10           1e-10           1e-10           1e-10
v  k                    0.0016836        0.023813        0.021511         0.02361
v  omega                   97.918      2.1748e+10      1.5514e+09      1.0608e+08
v  scalar1                      0               0               0               0
v  TurbVisc               0.24319         0.24319         0.24319         0.24319
v  CourantNb                    0               0               0               0
v  FourierNb             0.012526          99.986          15.466          1.6454
v  total_pressure       1.467e+05      4.8545e+07       2.956e+07      1.0385e+07
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012526          99.986          15.466          1.6454


 TIME FOR THE TIME STEP                1:        0.40558E+01

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


 INSTANT    0.100000000E-04   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.311038968E-04
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20142E+00 0.14979E+01
   Friction velocity        uet   :  0.26627E+00 0.12286E+01
   Friction velocity        uk    :  0.45834E+00 0.21261E+01
   Dimensionless distance   yplus :  0.11431E+01 0.52517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :        108
   Total number of wall faces                   :       1140
------------------------------------------------------------



@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.16937E-11
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.8956E-04


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13474E-01      23   0.10430E-03   0.16233E+06 0.55990E+05 
c  Velocity[X]                                      0.16078E+06 
c  Velocity[Y]                                      0.15452E+04 
c  Velocity[Z]                                      0.40249E-01 
c  Pressure     0.71497E-08    3171   0.16262E+00   0.10662E+01 0.20000E+06 
c  Void Fractio 0.10062E-08      31   0.38017E-08   0.00000E+00 0.00000E+00 
c  k            0.29866E-03      20   0.42072E-04   0.44838E+01 0.41140E+05 
c  omega        0.85121E+10       3   0.35380E-06   0.44658E+23 0.19994E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction     -0.00029411                         57000
a  k                 -1.9596e-06                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             1.0637          13.078           6.208          2.7048
v  Velocity[Y]            -1.2363          3.3491       -0.079753        -0.16975
v  Velocity[Z]           -0.16962         0.19997      3.8932e-07     -8.6297e-09
v  ǁVelocityǁ              1.0685          13.254          6.2464          2.7171
v  Pressure            1.6762e+05        1.86e+07      1.5369e+07      7.3587e+06
v  Void Fraction            1e-10           1e-10           1e-10           1e-10
v  k                   7.7172e-08        0.024666        0.014027        0.022409
v  omega                   91.457      1.0875e+10      7.7597e+08       5.308e+07
v  scalar1                      0               0               0               0
v  TurbVisc            7.9839e-11         0.24319        0.017036         0.14637
v  CourantNb            0.0015569          2.4688         0.67632        0.084337
v  FourierNb            0.0012737            1.08         0.13913        0.099673
v  total_pressure      1.6762e+05        1.86e+07      1.5369e+07      7.3587e+06
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013916          2.7081         0.81545         0.18401


 TIME FOR THE TIME STEP                2:        0.20706E+01

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


 INSTANT    0.150000000E-04   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.679450233E-04
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39978E+00 0.14881E+01
   Friction velocity        uet   :  0.25843E+00 0.12916E+01
   Friction velocity        uk    :  0.65221E+00 0.22098E+01
   Dimensionless distance   yplus :  0.16266E+01 0.53501E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          2
   Nb of faces within the viscous sub-layer     :         69
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.22605E-06
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.8577E-09


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33105E-01      30   0.75572E-04   0.46151E+06 0.68900E+05 
c  Velocity[X]                                      0.45811E+06 
c  Velocity[Y]                                      0.34047E+04 
c  Velocity[Z]                                      0.15135E-01 
c  Pressure     0.31568E-08    3030   0.42076E-01   0.73501E+00 0.91715E+05 
c  Void Fractio 0.94763E-14       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  k            0.29935E-03      21   0.26634E-07   0.90968E-01 0.58753E+04 
c  omega        0.21289E+10       4   0.38020E-06   0.11164E+23 0.19988E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -5.9134e-06                            28
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             2.1277          14.403          7.1028          4.1677
v  Velocity[Y]            -1.4334           4.088        -0.11944        -0.28706
v  Velocity[Z]          -0.074015        0.083259      7.7973e-07       2.934e-09
v  ǁVelocityǁ              2.1391          14.735          7.1466          4.1857
v  Pressure            3.1401e+05      2.7872e+07      2.4926e+07      1.4093e+07
v  Void Fraction            1e-10           1e-10           1e-10           1e-10
v  k                   1.9198e-11        0.024796        0.013518        0.022272
v  omega                   97.912       5.438e+09      3.8824e+08      2.6577e+07
v  scalar1                      0               0               0               0
v  TurbVisc            8.3298e-15          0.2432        0.015633         0.13587
v  CourantNb            0.0031736          3.5491         0.79548         0.10176
v  FourierNb            0.0016674         0.98433         0.13316        0.091593
v  total_pressure      3.1401e+05      2.7872e+07      2.4926e+07      1.4093e+07
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016111          3.8758         0.92864         0.19335


 TIME FOR THE TIME STEP                3:        0.20014E+01

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


 INSTANT    0.200000000E-04   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157508592E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60262E+00 0.14967E+01
   Friction velocity        uet   :  0.31965E+00 0.13364E+01
   Friction velocity        uk    :  0.92592E+00 0.22500E+01
   Dimensionless distance   yplus :  0.23093E+01 0.54363E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          2
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1068E-10


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63916E-01      30   0.42093E-04   0.15243E+03 0.12488E+04 
c  Velocity[X]                                      0.14709E+03 
c  Velocity[Y]                                      0.53279E+01 
c  Velocity[Z]                                      0.45167E-02 
c  Pressure     0.20531E-08    3315   0.34482E+00   0.68250E+00 0.16783E+08 
c  Void Fractio 0.11199E-14       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  k            0.30830E-03      21   0.22624E-07   0.25774E-01 0.31319E+04 
c  omega        0.53265E+09       4   0.57994E-05   0.27912E+22 0.19977E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.1556e-05                            57
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             1.2949          14.274          7.0927          4.1806
v  Velocity[Y]            -1.4164          4.0034        -0.11963        -0.28792
v  Velocity[Z]          -0.022671        0.030082      6.0434e-07      3.7092e-09
v  ǁVelocityǁ              1.2971          14.559          7.1366          4.1987
v  Pressure                 56366      3.3417e+05      2.7488e+05      1.7806e+05
v  Void Fraction            1e-10           1e-10           1e-10           1e-10
v  k                   1.3392e-13        0.024745        0.013299        0.022205
v  omega                   97.908      2.7196e+09      1.9437e+08      1.3324e+07
v  scalar1                      0               0               0               0
v  TurbVisc            4.1437e-18         0.24322         0.01526         0.13096
v  CourantNb            0.0062381          4.2642         0.88931         0.11917
v  FourierNb            0.0019865          1.0359          0.1302        0.088533
v  total_pressure           56366      3.3417e+05      2.7488e+05      1.7806e+05
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015428          4.5538          1.0195          0.2077


 TIME FOR THE TIME STEP                4:        0.21370E+01

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


 INSTANT    0.250000000E-04   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157509439E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19093E+00 0.14998E+01
   Friction velocity        uet   :  0.30475E+00 0.12597E+01
   Friction velocity        uk    :  0.71732E+00 0.21702E+01
   Dimensionless distance   yplus :  0.17890E+01 0.52437E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :         12
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1569E-11


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43550E-01      23   0.54050E-04   0.72051E+02 0.86027E+03 
c  Velocity[X]                                      0.69576E+02 
c  Velocity[Y]                                      0.24740E+01 
c  Velocity[Z]                                      0.29471E-03 
c  Pressure     0.21955E-08    2830   0.38793E-01   0.91097E+00 0.77380E+06 
c  Void Fractio 0.12344E-14       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  k            0.30369E-03      20   0.25687E-07   0.12290E-01 0.21648E+04 
c  omega        0.13338E+09       5   0.85539E-05   0.69777E+21 0.19953E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -2.048e-05                            85
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.95324          14.027            7.07          4.1715
v  Velocity[Y]            -1.3753          3.8857        -0.11898        -0.28738
v  Velocity[Z]          -0.010357        0.013998      2.2375e-07     -1.0666e-09
v  ǁVelocityǁ             0.95772          14.142          7.1136          4.1895
v  Pressure           -2.2744e+05           57317     -1.1927e+05          -23227
v  Void Fraction            1e-10           1e-10           1e-10           1e-10
v  k                   1.9057e-15        0.024632         0.01317        0.022161
v  omega                   97.905      1.3603e+09      9.7424e+07      6.6959e+06
v  scalar1                      0               0               0               0
v  TurbVisc            9.4607e-20         0.24322        0.015227         0.13076
v  CourantNb            0.0056502          4.6165         0.88693         0.11921
v  FourierNb            0.0024905          0.9475         0.12996        0.087799
v  total_pressure     -2.2744e+05           57317     -1.1927e+05          -23227
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015575          4.9061          1.0169         0.20701


 TIME FOR THE TIME STEP                5:        0.19292E+01

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


 INSTANT    0.300000000E-04   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157509452E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.15082E+01
   Friction velocity        uet   :  0.29700E+00 0.12127E+01
   Friction velocity        uk    :  0.61952E+00 0.21179E+01
   Dimensionless distance   yplus :  0.15451E+01 0.51171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         22
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.90545E-09
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1519E-06


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43157E-01      22   0.52971E-04   0.37424E+02 0.62024E+03 
c  Velocity[X]                                      0.36087E+02 
c  Velocity[Y]                                      0.13372E+01 
c  Velocity[Z]                                      0.57170E-04 
c  Pressure     0.72483E-09    2509   0.18919E-01   0.38252E+00 0.39923E+06 
c  Void Fractio 0.31631E-11      31   0.54783E-08   0.10295E-09 0.19987E+06 
c  k            0.30154E-03      20   0.44673E-07   0.77472E-02 0.17200E+04 
c  omega        0.33469E+08       6   0.15999E-06   0.17441E+21 0.19904E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction       -5.52e-07                         32435
a  k                 -3.6512e-05                            96
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.82348          13.855          7.0575          4.1692
v  Velocity[Y]            -1.3583           3.753        -0.11868        -0.28725
v  Velocity[Z]         -0.0057322       0.0069135      1.3039e-07     -9.5483e-10
v  ǁVelocityǁ             0.82765          14.079          7.1009          4.1872
v  Pressure                -86697           56460          6262.8           31443
v  Void Fraction            1e-10      1.1249e-06      4.2902e-08      3.4939e-09
v  k                   1.2064e-18        0.024679          0.0131        0.022129
v  omega                   97.902      6.8071e+08      4.8944e+07      3.3801e+06
v  scalar1                      0               0               0               0
v  TurbVisc            3.4464e-21         0.24322        0.015219         0.13086
v  CourantNb            0.0037202          4.7139         0.88539         0.11919
v  FourierNb            0.0032023         0.88563         0.12964        0.087335
v  total_pressure          -86697           56460          6262.8           31443
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015659          5.0035           1.015         0.20652


 TIME FOR THE TIME STEP                6:        0.17725E+01

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


 INSTANT    0.350000000E-04   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157360105E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.15182E+01
   Friction velocity        uet   :  0.29119E+00 0.12011E+01
   Friction velocity        uk    :  0.57593E+00 0.20985E+01
   Dimensionless distance   yplus :  0.14364E+01 0.50703E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         30
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.27517E-08
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.6414E-06


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43199E-01      21   0.57154E-04   0.27818E+02 0.53487E+03 
c  Velocity[X]                                      0.26838E+02 
c  Velocity[Y]                                      0.97933E+00 
c  Velocity[Z]                                      0.13266E-04 
c  Pressure     0.54893E-09    2068   0.18903E-02   0.32406E+00 0.75868E+05 
c  Void Fractio 0.17829E-10      44   0.51068E-08   0.17295E-03 0.19993E+06 
c  k            0.30029E-03      20   0.78735E-07   0.68942E-02 0.16235E+04 
c  omega        0.84432E+07       8   0.15729E-06   0.43572E+20 0.19793E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction     -8.7098e-05                         53765
a  k                 -6.3116e-05                            89
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.74246           13.84           7.046           4.168
v  Velocity[Y]            -1.3307          3.7792        -0.11709        -0.28698
v  Velocity[Z]         -0.0034088       0.0040372      1.0266e-07     -1.6842e-10
v  ǁVelocityǁ             0.74625          14.032          7.0895           4.186
v  Pressure                -66127           59352           17924           49261
v  Void Fraction            1e-10       0.0078996      2.0684e-05      6.4174e-07
v  k                   5.3786e-20         0.02481         0.01309        0.022105
v  omega                   97.899      3.4094e+08      2.4695e+07      1.7206e+06
v  scalar1                      0               0               0               0
v  TurbVisc            5.5631e-24         0.24322        0.015164         0.13064
v  CourantNb            0.0031704          4.7602         0.88388         0.11917
v  FourierNb            0.0041717         0.86489         0.12935        0.086717
v  total_pressure          -66127           59352           17924           49261
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015712          5.0498          1.0132         0.20589


 TIME FOR THE TIME STEP                7:        0.15570E+01

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


 INSTANT    0.400000000E-04   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157357623E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.15304E+01
   Friction velocity        uet   :  0.28538E+00 0.11695E+01
   Friction velocity        uk    :  0.54688E+00 0.20557E+01
   Dimensionless distance   yplus :  0.13639E+01 0.49668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         38
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.92887E-08
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1912E-05


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43225E-01      22   0.52992E-04   0.44265E+02 0.67481E+03 
c  Velocity[X]                                      0.30433E+02 
c  Velocity[Y]                                      0.13832E+02 
c  Velocity[Z]                                      0.34662E-05 
c  Pressure     0.58598E-07    1933   0.12037E-03   0.10046E+01 0.21013E+05 
c  Void Fractio 0.74768E-09      47   0.39094E-08   0.13165E+00 0.19625E+06 
c  k            0.29941E-03      20   0.13511E-06   0.10809E-01 0.20336E+04 
c  omega        0.21634E+07      10   0.25165E-06   0.10859E+20 0.19527E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction        -0.08179                         55512
a  k                 -2.4699e-05                            88
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.67691          14.402          7.0346          4.1672
v  Velocity[Y]            -1.3463          4.9694        -0.11398        -0.28693
v  Velocity[Z]         -0.0023453       0.0024878      8.5908e-08      3.3525e-10
v  ǁVelocityǁ             0.68035           14.54          7.0783          4.1852
v  Pressure               -1588.5           59128           27969           49796
v  Void Fraction            1e-10         0.66009      0.00019823      2.8941e-06
v  k                   1.5405e-22         0.04129        0.013162        0.022089
v  omega                   97.895      1.7107e+08      1.2562e+07      8.8948e+05
v  scalar1                      0               0               0               0
v  TurbVisc            3.6979e-25         0.24323        0.015133         0.13057
v  CourantNb            0.0026351          4.8436         0.88259         0.11915
v  FourierNb            0.0052575         0.87632         0.12897        0.086212
v  total_pressure         -1588.5           59128           27969           49796
v  Density Old               1000            1000            1000            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015793          5.1332          1.0116         0.20536


 TIME FOR THE TIME STEP                8:        0.15086E+01

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


 INSTANT    0.450000000E-04   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157324729E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.15483E+01
   Friction velocity        uet   :  0.28144E+00 0.10577E+01
   Friction velocity        uk    :  0.52218E+00 0.19261E+01
   Dimensionless distance   yplus :  0.13023E+01 0.46956E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         45
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.31320E-08
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.3330E-05


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43221E-01      28   0.55749E-04   0.37813E+02 0.62373E+03 
c  Velocity[X]                                      0.25774E+02 
c  Velocity[Y]                                      0.12040E+02 
c  Velocity[Z]                                      0.96049E-06 
c  Pressure     0.29458E-07    1860   0.48625E-03   0.10185E+01 0.12422E+05 
c  Void Fractio 0.13768E-08      47   0.39111E-08   0.16496E+00 0.11410E+06 
c  k            0.29877E-03      20   0.22493E-06   0.27570E-01 0.32480E+04 
c  omega        0.58183E+06      13   0.41390E-06   0.26807E+19 0.18817E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction         -0.1021                         56355
a  k                 -4.4715e-05                            68
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.62567          13.683          7.0257          4.1667
v  Velocity[Y]            -1.3145          5.7982        -0.11145        -0.28689
v  Velocity[Z]         -0.0019783       0.0019598      8.0528e-08      7.5265e-10
v  ǁVelocityǁ             0.62884          13.739          7.0695          4.1848
v  Pressure               -140.77           58973           33867           51422
v  Void Fraction            1e-10         0.90705      0.00049504      6.9606e-06
v  k                   1.4066e-23        0.075803        0.013367         0.02208
v  omega                   97.892      8.6731e+07      6.4847e+06      4.7341e+05
v  scalar1                      0               0               0               0
v  TurbVisc            2.1007e-27         0.24323        0.015116          0.1305
v  CourantNb            0.0023126          7.9839         0.88206         0.11912
v  FourierNb            0.0052846         0.87808         0.12876        0.085752
v  total_pressure         -140.77           58973           33867           51422
v  Density Old             992.11            1000          999.98            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015836          8.3131          1.0108         0.20487


 TIME FOR THE TIME STEP                9:        0.14828E+01

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


 INSTANT    0.500000000E-04   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157297963E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.15697E+01
   Friction velocity        uet   :  0.27826E+00 0.10326E+01
   Friction velocity        uk    :  0.50202E+00 0.19322E+01
   Dimensionless distance   yplus :  0.12521E+01 0.44093E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         54
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.63804E-08
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.3224E-05


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43221E-01      28   0.44843E-04   0.41919E+02 0.65657E+03 
c  Velocity[X]                                      0.25355E+02 
c  Velocity[Y]                                      0.16564E+02 
c  Velocity[Z]                                      0.26510E-06 
c  Pressure     0.30795E-07    2070   0.75944E-03   0.10056E+01 0.36836E+05 
c  Void Fractio 0.15615E-08      46   0.57505E-08   0.15734E+00 0.81403E+05 
c  k            0.29825E-03      19   0.45011E-06   0.83740E-01 0.56556E+04 
c  omega        0.18157E+06      15   0.36615E-05   0.63866E+18 0.16720E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction         -1.9813                         55735
a  k                 -7.4907e-05                            16
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.58509          13.094           7.019          4.1673
v  Velocity[Y]            -1.9321          3.6674        -0.11607        -0.28719
v  Velocity[Z]         -0.0016613       0.0017612      7.7354e-08      9.9916e-10
v  ǁVelocityǁ             0.58804          13.183          7.0627          4.1854
v  Pressure                1786.4           80628           53354           60212
v  Void Fraction            1e-10         0.92905      0.00076713      1.0911e-05
v  k                        1e-24         0.20612        0.013806         0.02208
v  omega                   97.889      9.2036e+07      3.4407e+06      2.6675e+05
v  scalar1                      0               0               0               0
v  TurbVisc            3.7745e-28         0.24323        0.015092         0.13042
v  CourantNb            0.0020803          7.8282         0.88237         0.11914
v  FourierNb            0.0053118         0.88305         0.12852        0.085306
v  total_pressure          1786.4           80628           53354           60212
v  Density Old             340.57            1000           999.8            1000


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015845          8.2305          1.0109         0.20445


 TIME FOR THE TIME STEP               10:        0.16447E+01

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


 INSTANT    0.550000000E-04   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157315401E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.17245E+01
   Friction velocity        uet   :  0.27472E+00 0.10085E+01
   Friction velocity        uk    :  0.48547E+00 0.17593E+01
   Dimensionless distance   yplus :  0.12108E+01 0.41369E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         64
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.77621E-08
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1806E-05


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43242E-01      29   0.57447E-04   0.49942E+02 0.71637E+03 
c  Velocity[X]                                      0.29038E+02 
c  Velocity[Y]                                      0.20903E+02 
c  Velocity[Z]                                      0.83793E-07 
c  Pressure     0.10495E-08    3210   0.24484E-01   0.11609E+01 0.36541E+05 
c  Void Fractio 0.16614E-08      47   0.37035E-08   0.14005E+00 0.67141E+05 
c  k            0.29790E-03      19   0.20373E-05   0.26439E+00 0.10013E+05 
c  omega        0.92344E+05      16   0.96072E-06   0.15129E+18 0.12403E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction         -1.5281                         54921
a  k                 -7.2435e-07                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             0.5514           12.86          7.0105          4.1691
v  Velocity[Y]            -4.3601          3.4748        -0.11822         -0.2874
v  Velocity[Z]          -0.001505       0.0016787      8.1091e-08      1.2668e-09
v  ǁVelocityǁ             0.55418          12.941          7.0544          4.1871
v  Pressure                  1810           97274           74883           71060
v  Void Fraction            1e-10         0.90263      0.00090898      1.3114e-05
v  k                        1e-24         0.65772        0.014648        0.022095
v  omega                   97.886      4.9711e+07      1.9142e+06      1.6576e+05
v  scalar1                      0               0               0               0
v  TurbVisc            5.2006e-29         0.24324        0.015047         0.13033
v  CourantNb            0.0019046          5.8945         0.88221         0.11917
v  FourierNb             0.005337         0.87327         0.12804         0.08484
v  total_pressure            1810           97274           74883           71060
v  Density Old             93.861            1000          999.51          999.99


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015858          6.1888          1.0103         0.20401


 TIME FOR THE TIME STEP               11:        0.22032E+01

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


 INSTANT    0.600000000E-04   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157393330E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.17379E+01
   Friction velocity        uet   :  0.27936E+00 0.10085E+01
   Friction velocity        uk    :  0.47128E+00 0.17801E+01
   Dimensionless distance   yplus :  0.11754E+01 0.42223E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         76
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.47857E-06
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.4510E-06


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43284E-01      29   0.61677E-04   0.45050E+02 0.68011E+03 
c  Velocity[X]                                      0.31727E+02 
c  Velocity[Y]                                      0.13323E+02 
c  Velocity[Z]                                      0.32554E-07 
c  Pressure     0.12170E-08    2438   0.95266E-02   0.11391E+01 0.25818E+04 
c  Void Fractio 0.14815E-08      42   0.46244E-08   0.90850E-01 0.52186E+05 
c  k            0.29767E-03      20   0.24818E-05   0.68521E+00 0.15950E+05 
c  omega        0.78824E+05      16   0.81753E-06   0.53428E+17 0.86598E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction        -0.89639                         54582
a  k                   3.848e-25                             1
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.52325          13.264          7.0035          4.1709
v  Velocity[Y]            -3.9195          3.5216         -0.1171        -0.28754
v  Velocity[Z]         -0.0014904       0.0016442      8.5646e-08      1.4785e-09
v  ǁVelocityǁ             0.52589          13.367          7.0471          4.1889
v  Pressure                1915.7      1.0477e+05           76465           71670
v  Void Fraction            1e-10         0.91175      0.00094757      1.3656e-05
v  k                        1e-24          1.1799        0.016106        0.022128
v  omega                   97.882      6.2508e+07      1.1517e+06      1.1678e+05
v  scalar1                      0               0               0               0
v  TurbVisc            9.8146e-29         0.24324         0.01503         0.13025
v  CourantNb            0.0017778          5.0647           0.881         0.11918
v  FourierNb            0.0053524         0.89812         0.12801        0.084459
v  total_pressure          1915.7      1.0477e+05           76465           71670
v  Density Old             71.881            1000          999.23          999.99


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015867          5.3252           1.009         0.20364


 TIME FOR THE TIME STEP               12:        0.18111E+01

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


 INSTANT    0.650000000E-04   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157473977E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.17680E+01
   Friction velocity        uet   :  0.27951E+00 0.11687E+01
   Friction velocity        uk    :  0.45909E+00 0.18705E+01
   Dimensionless distance   yplus :  0.11450E+01 0.45195E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         87
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.70445E-06
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.2291E-06


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43311E-01      26   0.50480E-04   0.17553E+02 0.42441E+03 
c  Velocity[X]                                      0.14632E+02 
c  Velocity[Y]                                      0.29209E+01 
c  Velocity[Z]                                      0.29673E-07 
c  Pressure     0.98727E-09    3118   0.96099E-02   0.10291E+01 0.26171E+05 
c  Void Fractio 0.14919E-08      41   0.39806E-08   0.79285E-01 0.48403E+05 
c  k            0.29771E-03      22   0.19609E-05   0.13564E+01 0.21898E+05 
c  omega        0.79985E+05      17   0.13372E-05   0.30071E+17 0.68530E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction        -0.68847                         54371
a  k                  8.6502e-25                             1
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.40583          13.225           6.997           4.172
v  Velocity[Y]            -4.1626           3.496        -0.11699        -0.28764
v  Velocity[Z]         -0.0014412       0.0016049       9.058e-08       1.664e-09
v  ǁVelocityǁ             0.15053          13.291          7.0406            4.19
v  Pressure                1906.1           85381           62157           64635
v  Void Fraction            1e-10         0.93068      0.00097347      1.3966e-05
v  k                        1e-24          1.6213        0.018333        0.022186
v  omega                   97.879      9.7973e+07      7.7429e+05           90427
v  scalar1                      0               0               0               0
v  TurbVisc             1.773e-28         0.24324        0.015011         0.13016
v  CourantNb            0.0016672          4.6298         0.87883         0.11919
v  FourierNb            0.0053757         0.92302         0.12799        0.084094
v  total_pressure          1906.1           85381           62157           64635
v  Density Old             98.271            1000          999.09          999.99


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015885          4.8577          1.0068         0.20328


 TIME FOR THE TIME STEP               13:        0.20547E+01

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


 INSTANT    0.700000000E-04   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157518226E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.19570E+01
   Friction velocity        uet   :  0.25835E+00 0.10786E+01
   Friction velocity        uk    :  0.24894E+00 0.17620E+01
   Dimensionless distance   yplus :  0.61679E+00 0.42573E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        106
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.78714E-06
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1586E-06


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43317E-01      24   0.45856E-04   0.17485E+02 0.42347E+03 
c  Velocity[X]                                      0.14876E+02 
c  Velocity[Y]                                      0.26091E+01 
c  Velocity[Z]                                      0.18364E-07 
c  Pressure     0.82078E-09    2274   0.68660E-02   0.95199E+00 0.78130E+03 
c  Void Fractio 0.14759E-08      38   0.48142E-08   0.66082E-01 0.44462E+05 
c  k            0.29765E-03      22   0.26111E-05   0.19696E+01 0.25447E+05 
c  omega        0.81538E+05      17   0.17459E-05   0.16700E+18 0.12865E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction        -0.50438                         54212
a  k                  -2.327e-09                             2
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.1012          13.056          6.9905           4.173
v  Velocity[Y]             -4.536          3.4856        -0.11686        -0.28774
v  Velocity[Z]         -0.0014404       0.0016073      9.4219e-08      1.8019e-09
v  ǁVelocityǁ             0.31561          13.147          7.0342          4.1911
v  Pressure                1876.8           84676           61805           64504
v  Void Fraction            1e-10         0.95208      0.00099298      1.4242e-05
v  k                        1e-24          1.6869        0.021064        0.022245
v  omega                   97.876       1.416e+08      6.0489e+05           84209
v  scalar1                      0               0               0               0
v  TurbVisc            2.1371e-29         0.24325        0.014972         0.13006
v  CourantNb                    0          5.1414         0.87804         0.11921
v  FourierNb            0.0053983         0.93305         0.12787        0.083697
v  total_pressure          1876.8           84676           61805           64504
v  Density Old             89.165            1000          999.05          999.99


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.0159          5.4646          1.0059         0.20291


 TIME FOR THE TIME STEP               14:        0.16493E+01

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


 INSTANT    0.750000000E-04   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157562665E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.20495E+01
   Friction velocity        uet   :  0.29532E+00 0.10718E+01
   Friction velocity        uk    :  0.33918E+00 0.17127E+01
   Dimensionless distance   yplus :  0.84021E+00 0.41382E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        133
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.83619E-06
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1373E-06


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43333E-01      22   0.43878E-04   0.17993E+02 0.42946E+03 
c  Velocity[X]                                      0.15450E+02 
c  Velocity[Y]                                      0.25430E+01 
c  Velocity[Z]                                      0.20421E-07 
c  Pressure     0.75254E-09    2451   0.61934E-02   0.83167E+00 0.18246E+04 
c  Void Fractio 0.14193E-08      36   0.47229E-08   0.61694E-01 0.43416E+05 
c  k            0.29758E-03      23   0.20981E-05   0.17790E+01 0.23367E+05 
c  omega        0.11122E+06      17   0.13406E-05   0.31207E+18 0.14818E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction        -0.54004                         54075
a  k                 -0.00018083                             3
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.4642          13.032          6.9843          4.1741
v  Velocity[Y]            -3.9566          3.4679        -0.11666        -0.28784
v  Velocity[Z]         -0.0014227       0.0015892       9.572e-08      1.8682e-09
v  ǁVelocityǁ             0.12735          13.123          7.0281          4.1922
v  Pressure                1855.7           85782           62861           64928
v  Void Fraction            1e-10         0.96434       0.0010119      1.4551e-05
v  k                        1e-24          1.8444        0.023529        0.022281
v  omega                   97.873      1.7866e+08      5.4898e+05           84165
v  scalar1                      0               0               0               0
v  TurbVisc            2.1376e-29         0.24325        0.014924         0.12993
v  CourantNb                    0          5.1036         0.87718         0.11923
v  FourierNb            0.0054197         0.94422         0.12781        0.083294
v  total_pressure          1855.7           85782           62861           64928
v  Density Old             70.252            1000          999.03          999.99


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015915          5.3923           1.005         0.20252


 TIME FOR THE TIME STEP               15:        0.17605E+01

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


 INSTANT    0.800000000E-04   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157609148E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.20985E+01
   Friction velocity        uet   :  0.24722E+00 0.10867E+01
   Friction velocity        uk    :  0.28563E+00 0.16881E+01
   Dimensionless distance   yplus :  0.70853E+00 0.40787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        156
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.58112E-06
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.2210E-06


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43351E-01      22   0.43029E-04   0.18589E+02 0.43638E+03 
c  Velocity[X]                                      0.15515E+02 
c  Velocity[Y]                                      0.30733E+01 
c  Velocity[Z]                                      0.12154E-07 
c  Pressure     0.73607E-09    2397   0.63917E-02   0.76209E+00 0.17344E+04 
c  Void Fractio 0.14508E-08      35   0.39664E-08   0.30226E-01 0.30657E+05 
c  k            0.29753E-03      24   0.69343E-05   0.11490E+01 0.18455E+05 
c  omega        0.13724E+06      16   0.39042E-05   0.29598E+18 0.14415E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction         -1.4746                         53941
a  k                 -0.00021454                            13
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4647          13.034          6.9785          4.1752
v  Velocity[Y]             -4.142          3.4483        -0.11645        -0.28795
v  Velocity[Z]         -0.0014198       0.0015771      9.6074e-08      1.8946e-09
v  ǁVelocityǁ            0.096464          13.195          7.0224          4.1933
v  Pressure                1843.5           86897           63915           65363
v  Void Fraction            1e-10         0.96779       0.0010437      1.5034e-05
v  k                        1e-24          1.9398        0.024994         0.02229
v  omega                    97.87      1.9344e+08      5.1632e+05           80245
v  scalar1                      0               0               0               0
v  TurbVisc            2.1378e-29         0.24325        0.014876         0.12981
v  CourantNb                    0          5.0351         0.87636         0.11925
v  FourierNb            0.0054398          0.9548         0.12779          0.0829
v  total_pressure          1843.5           86897           63915           65363
v  Density Old              48.87            1000          999.01          999.99


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01593          5.3271          1.0041         0.20215


 TIME FOR THE TIME STEP               16:        0.17074E+01

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


 INSTANT    0.850000000E-04   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157658369E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.21104E+01
   Friction velocity        uet   :  0.15873E+00 0.12182E+01
   Friction velocity        uk    :  0.15867E+00 0.16930E+01
   Dimensionless distance   yplus :  0.39306E+00 0.40906E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        214
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.15807E-05
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.3945E-11


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43369E-01      21   0.42029E-04   0.28821E+02 0.54320E+03 
c  Velocity[X]                                      0.25325E+02 
c  Velocity[Y]                                      0.34956E+01 
c  Velocity[Z]                                      0.11169E-07 
c  Pressure     0.86375E-09    2362   0.79000E-02   0.92866E+00 0.19206E+04 
c  Void Fractio 0.12625E-08      35   0.52585E-08   0.36632E-01 0.34761E+05 
c  k            0.29702E-03      24   0.46926E-05   0.23224E+01 0.26451E+05 
c  omega        0.13000E+06      16   0.27560E-05   0.67713E+18 0.16591E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction      8.0972e-11                         53819
a  k                 -0.00010014                            12
a  omega             -4.6916e+06                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4838          13.036          6.9722          4.1764
v  Velocity[Y]            -2.6561          3.4207        -0.11587        -0.28805
v  Velocity[Z]         -0.0014193        0.001568      9.1759e-08      1.8046e-09
v  ǁVelocityǁ             0.25193          13.279          7.0164          4.1945
v  Pressure                1837.3           88358           65269           65779
v  Void Fraction            1e-10           0.967       0.0010569      1.5295e-05
v  k                        1e-24          2.0387        0.025507        0.022257
v  omega                   97.866      2.0599e+08      6.1904e+05           89411
v  scalar1                      0               0               0               0
v  TurbVisc            2.1379e-29         0.24326        0.014828         0.12969
v  CourantNb                    0          5.0023         0.87557         0.11927
v  FourierNb            0.0054587         0.96525         0.12777        0.082522
v  total_pressure          1837.3           88358           65269           65779
v  Density Old             36.621            1000          998.99          999.99


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015944          5.2938          1.0033          0.2018


 TIME FOR THE TIME STEP               17:        0.16890E+01

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


 INSTANT    0.900000000E-04   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157709748E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.21193E+01
   Friction velocity        uet   :  0.29471E+00 0.13433E+01
   Friction velocity        uk    :  0.33034E+00 0.16748E+01
   Dimensionless distance   yplus :  0.81832E+00 0.40467E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        272
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.17299E-05
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.3826E-11


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43387E-01      21   0.41751E-04   0.60662E+02 0.78783E+03 
c  Velocity[X]                                      0.58570E+02 
c  Velocity[Y]                                      0.20926E+01 
c  Velocity[Z]                                      0.24578E-07 
c  Pressure     0.67349E-09    1940   0.12460E-01   0.74060E+00 0.10363E+04 
c  Void Fractio 0.11806E-08      35   0.41827E-08   0.17891E-01 0.25025E+05 
c  k            0.29651E-03      24   0.32297E-05   0.26985E+01 0.28970E+05 
c  omega        0.17600E+06      15   0.27784E-05   0.68692E+18 0.16343E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction      8.0942e-11                         53694
a  k                 -3.7406e-25                            10
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.028          13.048          6.9655          4.1776
v  Velocity[Y]            -1.6614          3.3942        -0.11528        -0.28815
v  Velocity[Z]         -0.0013417       0.0015121       8.887e-08      1.7626e-09
v  ǁVelocityǁ            0.098339          26.143          7.0106          4.1957
v  Pressure                  1839           88488           65141           65522
v  Void Fraction            1e-10         0.95223       0.0010759      1.5621e-05
v  k                        1e-24          2.0399        0.025492        0.022205
v  omega                   12.363      2.2212e+08      6.8502e+05           91924
v  scalar1                      0               0               0               0
v  TurbVisc             2.138e-29         0.24326        0.014783         0.12957
v  CourantNb                    0           4.987         0.87454         0.11929
v  FourierNb            0.0054766         0.97536         0.12773        0.082157
v  total_pressure            1839           88488           65141           65522
v  Density Old             33.177            1000          998.96          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015958          5.2621          1.0023         0.20145


 TIME FOR THE TIME STEP               18:        0.14850E+01

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


 INSTANT    0.950000000E-04   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157759785E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.91872E+01 0.20906E+01
   Friction velocity        uet   :  0.17147E+00 0.26292E+01
   Friction velocity        uk    :  0.17144E+00 0.30479E+01
   Dimensionless distance   yplus :  0.42472E+00 0.73106E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :        313
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.20660E-05
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.3840E-11


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43404E-01      22   0.39548E-04   0.34329E+02 0.59248E+03 
c  Velocity[X]                                      0.33547E+02 
c  Velocity[Y]                                      0.78170E+00 
c  Velocity[Z]                                      0.15818E-07 
c  Pressure     0.54121E-09    2470   0.72385E-02   0.67643E+00 0.25553E+04 
c  Void Fractio 0.11242E-08      35   0.41064E-08   0.10594E-01 0.19651E+05 
c  k            0.29624E-03      24   0.29425E-05   0.18439E+01 0.24224E+05 
c  omega        0.16378E+06      15   0.31973E-05   0.45864E+18 0.14933E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction      8.1037e-11                         53579
a  k                 -1.0093e-05                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5218          13.018          6.9597          4.1787
v  Velocity[Y]            -1.6107          3.3959        -0.11492        -0.28825
v  Velocity[Z]         -0.0012921       0.0014425      8.4151e-08      1.6679e-09
v  ǁVelocityǁ             0.10864          13.127          7.0043          4.1968
v  Pressure                  1846           87028           63662           64856
v  Void Fraction            1e-10         0.91993       0.0010998      1.6009e-05
v  k                        1e-24          1.8854        0.025348        0.022163
v  omega                   1.9115      2.9574e+08      6.8534e+05           86298
v  scalar1                      0               0               0               0
v  TurbVisc             2.138e-29         0.24326         0.01474         0.12946
v  CourantNb           0.00059078          4.9692         0.87374         0.11932
v  FourierNb            0.0054934         0.96352         0.12765          0.0818
v  total_pressure            1846           87028           63662           64856
v  Density Old             33.968            1000          998.94          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015972          5.2721          1.0014         0.20112


 TIME FOR THE TIME STEP               19:        0.17515E+01

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


 INSTANT    0.100000000E-03   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157807061E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.19606E+01
   Friction velocity        uet   :  0.20047E+00 0.11427E+01
   Friction velocity        uk    :  0.20045E+00 0.16571E+01
   Dimensionless distance   yplus :  0.49659E+00 0.40039E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        341
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1733E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43420E-01      21   0.40565E-04   0.10915E+02 0.33399E+03 
c  Velocity[X]                                      0.10562E+02 
c  Velocity[Y]                                      0.35320E+00 
c  Velocity[Z]                                      0.22959E-07 
c  Pressure     0.32770E-09    2174   0.43829E-02   0.44732E+00 0.17126E+04 
c  Void Fractio 0.10261E-08      34   0.52233E-08   0.51837E-02 0.13877E+05 
c  k            0.29614E-03      23   0.58638E-05   0.10613E+01 0.18500E+05 
c  omega        0.12963E+06      15   0.59285E-05   0.22391E+18 0.12251E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.6254e-05                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2039          12.944          6.9538          4.1798
v  Velocity[Y]            -1.6032           3.399        -0.11459        -0.28834
v  Velocity[Z]         -0.0011887       0.0013357       8.536e-08      1.6819e-09
v  ǁVelocityǁ            0.053646          13.126          6.9983          4.1979
v  Pressure                1904.5           85963           62637           64432
v  Void Fraction       8.1119e-11         0.80492       0.0011287      1.6457e-05
v  k                   2.0105e-24           2.032        0.025171        0.022139
v  omega                   97.857      2.3023e+08      6.4036e+05           78698
v  scalar1                      0               0               0               0
v  TurbVisc            2.1381e-29         0.24327        0.014693         0.12934
v  CourantNb           0.00067642          4.9699         0.87313         0.11935
v  FourierNb            0.0055093          0.9474         0.12755        0.081446
v  total_pressure          1904.5           85963           62637           64432
v  Density Old             48.724            1000          998.93          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015985          5.2872          1.0007         0.20079


 TIME FOR THE TIME STEP               20:        0.16113E+01

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


 INSTANT    0.105000000E-03   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157852936E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18708E+01
   Friction velocity        uet   :  0.14501E+00 0.11411E+01
   Friction velocity        uk    :  0.14501E+00 0.16461E+01
   Dimensionless distance   yplus :  0.35915E+00 0.39771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        374
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1370E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43435E-01      21   0.39168E-04   0.83744E+01 0.29247E+03 
c  Velocity[X]                                      0.81709E+01 
c  Velocity[Y]                                      0.20354E+00 
c  Velocity[Z]                                      0.12457E-07 
c  Pressure     0.14847E-09    2591   0.22432E-02   0.19710E+00 0.25178E+04 
c  Void Fractio 0.10016E-08      36   0.43530E-08   0.26389E-02 0.99099E+04 
c  k            0.29608E-03      23   0.48938E-05   0.71467E+00 0.15269E+05 
c  omega        0.10125E+06      16   0.57227E-05   0.16874E+18 0.11101E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.6832e-05                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5948          12.915          6.9481          4.1808
v  Velocity[Y]            -1.6117          3.3677        -0.11426        -0.28843
v  Velocity[Z]         -0.0011727       0.0012834      8.5993e-08      1.6949e-09
v  ǁVelocityǁ            0.013578          13.026          6.9925           4.199
v  Pressure                1925.5           84388           61176           63801
v  Void Fraction        6.589e-11         0.78601       0.0011617      1.6961e-05
v  k                   4.5907e-24          1.8465        0.024961        0.022122
v  omega                   97.853      2.3328e+08      6.4863e+05           75554
v  scalar1                      0               0               0               0
v  TurbVisc            4.2987e-29         0.24327        0.014648         0.12923
v  CourantNb           0.00073305          4.9712         0.87249         0.11937
v  FourierNb             0.005524         0.93287         0.12745        0.081107
v  total_pressure          1925.5           84388           61176           63801
v  Density Old              80.99            1000           998.9          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015997          5.2845         0.99994         0.20048


 TIME FOR THE TIME STEP               21:        0.17924E+01

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


 INSTANT    0.110000000E-03   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157896236E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18704E+01
   Friction velocity        uet   :  0.55374E-01 0.11409E+01
   Friction velocity        uk    :  0.55372E-01 0.16356E+01
   Dimensionless distance   yplus :  0.13716E+00 0.39519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        405
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.8406E-14


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43449E-01      22   0.39309E-04   0.73472E+01 0.27388E+03 
c  Velocity[X]                                      0.71576E+01 
c  Velocity[Y]                                      0.18960E+00 
c  Velocity[Z]                                      0.24706E-07 
c  Pressure     0.10448E-09    2611   0.16969E-02   0.14155E+00 0.23141E+04 
c  Void Fractio 0.10163E-08      37   0.53471E-08   0.20376E-02 0.86737E+04 
c  k            0.29604E-03      23   0.28906E-05   0.59367E+00 0.13987E+05 
c  omega        0.96634E+05      15   0.54206E-05   0.12855E+18 0.10012E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.6758e-05                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3613          12.909          6.9423          4.1818
v  Velocity[Y]            -1.6129          3.3278        -0.11394        -0.28852
v  Velocity[Z]         -0.0011853        0.001262      9.1621e-08      1.8188e-09
v  ǁVelocityǁ            0.073831          12.975          6.9869          4.1999
v  Pressure                1926.2           82934           59865           63213
v  Void Fraction       5.3591e-11         0.79346       0.0011982      1.7519e-05
v  k                   9.7508e-24          1.7885        0.024709        0.022108
v  omega                    97.85       2.357e+08      6.5562e+05           73717
v  scalar1                      0               0               0               0
v  TurbVisc            9.8157e-29         0.24327        0.014605         0.12913
v  CourantNb           0.00076988          4.9831          0.8719         0.11939
v  FourierNb            0.0055379           0.918         0.12734        0.080781
v  total_pressure          1926.2           82934           59865           63213
v  Density Old             195.89            1000          998.87          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016009          5.2946         0.99924         0.20017


 TIME FOR THE TIME STEP               22:        0.18152E+01

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


 INSTANT    0.115000000E-03   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157937234E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18687E+01
   Friction velocity        uet   :  0.17339E+00 0.11407E+01
   Friction velocity        uk    :  0.17338E+00 0.16251E+01
   Dimensionless distance   yplus :  0.42964E+00 0.39266E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        432
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2627E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43463E-01      22   0.36515E-04   0.66150E+01 0.25981E+03 
c  Velocity[X]                                      0.64253E+01 
c  Velocity[Y]                                      0.18971E+00 
c  Velocity[Z]                                      0.16125E-07 
c  Pressure     0.81579E-10    2535   0.13650E-02   0.11279E+00 0.16106E+04 
c  Void Fractio 0.10382E-08      37   0.43938E-08   0.18442E-02 0.81878E+04 
c  k            0.29600E-03      23   0.10211E-04   0.49078E+00 0.12773E+05 
c  omega        0.92040E+05      15   0.14111E-04   0.10986E+18 0.93837E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -5.7812e-06                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.5254          12.876          6.9367          4.1827
v  Velocity[Y]              -1.62          3.3286        -0.11362        -0.28861
v  Velocity[Z]         -0.0011913       0.0012543      9.5622e-08      1.9082e-09
v  ǁVelocityǁ            0.067187          12.943          6.9814          4.2009
v  Pressure                1914.1           81844           58957           62814
v  Void Fraction        4.363e-11         0.81015       0.0012377      1.8128e-05
v  k                   1.9431e-23          1.7562        0.024482        0.022095
v  omega                   97.847      2.3837e+08      6.5331e+05           73125
v  scalar1                      0               0               0               0
v  TurbVisc            2.0848e-28         0.24328        0.014563         0.12903
v  CourantNb           0.00079262          5.0142         0.87135         0.11942
v  FourierNb            0.0055494         0.90619         0.12723        0.080466
v  total_pressure          1914.1           81844           58957           62814
v  Density Old             214.77            1000          998.84          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016018          5.3375         0.99858         0.19988


 TIME FOR THE TIME STEP               23:        0.17696E+01

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


 INSTANT    0.120000000E-03   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.157976531E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18671E+01
   Friction velocity        uet   :  0.16017E+00 0.11367E+01
   Friction velocity        uk    :  0.16016E+00 0.16167E+01
   Dimensionless distance   yplus :  0.39687E+00 0.39063E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        459
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1841E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43476E-01      22   0.38106E-04   0.59743E+01 0.24684E+03 
c  Velocity[X]                                      0.57992E+01 
c  Velocity[Y]                                      0.17513E+00 
c  Velocity[Z]                                      0.10748E-07 
c  Pressure     0.78178E-10    2502   0.15157E-02   0.10960E+00 0.16259E+04 
c  Void Fractio 0.10630E-08      37   0.44870E-08   0.18025E-02 0.80087E+04 
c  k            0.29598E-03      23   0.79586E-05   0.40046E+00 0.11580E+05 
c  omega        0.91585E+05      15   0.77300E-05   0.83098E+17 0.83535E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.0995e-07                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6801          12.847           6.931          4.1836
v  Velocity[Y]            -1.6302          3.3286        -0.11329         -0.2887
v  Velocity[Z]         -0.0012224       0.0012608      9.8352e-08      1.9637e-09
v  ǁVelocityǁ            0.018168          12.918          6.9759          4.2018
v  Pressure                1596.3           80754           58024           62422
v  Void Fraction       3.5554e-11         0.82645       0.0012796      1.8786e-05
v  k                   3.6675e-23          1.7249        0.024241        0.022084
v  omega                   97.844      2.4084e+08      6.6633e+05           71883
v  scalar1                      0               0               0               0
v  TurbVisc            4.1544e-28         0.24328        0.014523         0.12893
v  CourantNb           0.00080549          5.0325         0.87084         0.11944
v  FourierNb            0.0055603         0.89331         0.12712         0.08016
v  total_pressure          1596.3           80754           58024           62422
v  Density Old             207.33            1000           998.8          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016027          5.3345         0.99796          0.1996


 TIME FOR THE TIME STEP               24:        0.17639E+01

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


 INSTANT    0.125000000E-03   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158014333E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18653E+01
   Friction velocity        uet   :  0.64693E-01 0.11444E+01
   Friction velocity        uk    :  0.64689E-01 0.16072E+01
   Dimensionless distance   yplus :  0.16034E+00 0.38833E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        490
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.3155E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43489E-01      23   0.34969E-04   0.55278E+01 0.23739E+03 
c  Velocity[X]                                      0.53278E+01 
c  Velocity[Y]                                      0.20002E+00 
c  Velocity[Z]                                      0.22332E-07 
c  Pressure     0.16438E-08    2058   0.56621E-03   0.10299E+01 0.93234E+03 
c  Void Fractio 0.10933E-08      36   0.60630E-08   0.20352E-02 0.83926E+04 
c  k            0.29596E-03      22   0.28630E-05   0.34562E+00 0.10793E+05 
c  omega        0.88759E+05      15   0.59721E-05   0.73812E+17 0.79210E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.0635e-06                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7885          12.829          6.9255          4.1845
v  Velocity[Y]            -1.6365          3.3215        -0.11296        -0.28878
v  Velocity[Z]         -0.0012257       0.0012547      9.5861e-08      1.9185e-09
v  ǁVelocityǁ             0.10494          12.884          6.9705          4.2027
v  Pressure                1890.2           80140           57487           62200
v  Void Fraction        2.899e-11         0.88159       0.0013239      1.9493e-05
v  k                   6.6073e-23          1.7255        0.023959        0.022074
v  omega                   97.841      2.4436e+08      6.9038e+05           71232
v  scalar1                      0               0               0               0
v  TurbVisc            7.8416e-28         0.24328        0.014485         0.12884
v  CourantNb           0.00081199          5.0451         0.87033         0.11946
v  FourierNb            0.0055705         0.88158         0.12701         0.07986
v  total_pressure          1890.2           80140           57487           62200
v  Density Old             190.66            1000          998.76          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016035          5.3439         0.99734         0.19932


 TIME FOR THE TIME STEP               25:        0.15642E+01

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


 INSTANT    0.130000000E-03   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158051411E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18633E+01
   Friction velocity        uet   :  0.20700E+00 0.11405E+01
   Friction velocity        uk    :  0.20699E+00 0.16021E+01
   Dimensionless distance   yplus :  0.51304E+00 0.38709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        530
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.9006E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43501E-01      22   0.35297E-04   0.52040E+01 0.23028E+03 
c  Velocity[X]                                      0.50221E+01 
c  Velocity[Y]                                      0.18197E+00 
c  Velocity[Z]                                      0.12646E-07 
c  Pressure     0.14052E-09    2123   0.12062E-02   0.20562E+00 0.13834E+04 
c  Void Fractio 0.10944E-08      36   0.48593E-08   0.20905E-02 0.83751E+04 
c  k            0.29594E-03      23   0.28047E-05   0.36211E+00 0.11087E+05 
c  omega        0.88062E+05      17   0.50228E-05   0.77854E+17 0.80684E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -0.00020987                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7822          12.803          6.9199          4.1854
v  Velocity[Y]            -1.6408          3.2911        -0.11263        -0.28886
v  Velocity[Z]         -0.0011757       0.0012382      9.6725e-08      1.9425e-09
v  ǁVelocityǁ            0.021408          12.848          6.9651          4.2035
v  Pressure                1722.2           79218           56718           61861
v  Void Fraction       2.3657e-11         0.88869       0.0013702      2.0246e-05
v  k                   1.1434e-22          1.6868        0.023561        0.022064
v  omega                   97.838      2.4789e+08      7.5379e+05           71074
v  scalar1                      0               0               0               0
v  TurbVisc            1.4127e-27         0.24329        0.014447         0.12874
v  CourantNb           0.00081092          4.9679         0.86984         0.11948
v  FourierNb            0.0055802          0.8721         0.12689        0.079566
v  total_pressure          1722.2           79218           56718           61861
v  Density Old             174.38            1000          998.72          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016043           5.269         0.99673         0.19905


 TIME FOR THE TIME STEP               26:        0.15852E+01

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


 INSTANT    0.135000000E-03   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158087100E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18611E+01
   Friction velocity        uet   :  0.74076E-01 0.11397E+01
   Friction velocity        uk    :  0.74069E-01 0.15935E+01
   Dimensionless distance   yplus :  0.18358E+00 0.38502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        562
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1071E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43514E-01      22   0.39388E-04   0.48718E+01 0.22276E+03 
c  Velocity[X]                                      0.46793E+01 
c  Velocity[Y]                                      0.19247E+00 
c  Velocity[Z]                                      0.10515E-07 
c  Pressure     0.31849E-08    1619   0.20282E-03   0.10094E+01 0.43314E+03 
c  Void Fractio 0.11125E-08      35   0.50790E-08   0.33682E-02 0.10427E+05 
c  k            0.29593E-03      24   0.29235E-05   0.30370E+00 0.10184E+05 
c  omega        0.87754E+05      15   0.48223E-05   0.57777E+17 0.70798E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -0.0002372                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7836          12.775          6.9143          4.1862
v  Velocity[Y]            -1.6527          3.2829        -0.11231        -0.28894
v  Velocity[Z]         -0.0011755       0.0012385      9.7983e-08      1.9692e-09
v  ǁVelocityǁ            0.063798          12.788          6.9597          4.2044
v  Pressure                1894.3           78867           56455           61768
v  Void Fraction       1.9311e-11         0.89108       0.0014178      2.1045e-05
v  k                   1.9106e-22          1.6981        0.023117        0.022055
v  omega                   97.835      2.5803e+08      7.6527e+05           70421
v  scalar1                      0               0               0               0
v  TurbVisc            2.4448e-27         0.24329         0.01441         0.12865
v  CourantNb           0.00080797          4.9434          0.8693          0.1195
v  FourierNb            0.0055892         0.86345         0.12676        0.079279
v  total_pressure          1894.3           78867           56455           61768
v  Density Old             119.29            1000          998.68          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01605          5.2465         0.99606         0.19878


 TIME FOR THE TIME STEP               27:        0.13435E+01

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


 INSTANT    0.140000000E-03   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158122671E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18588E+01
   Friction velocity        uet   :  0.18362E+00 0.11390E+01
   Friction velocity        uk    :  0.18360E+00 0.15864E+01
   Dimensionless distance   yplus :  0.45495E+00 0.38329E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        609
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2632E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43526E-01      22   0.39075E-04   0.47577E+01 0.22008E+03 
c  Velocity[X]                                      0.45700E+01 
c  Velocity[Y]                                      0.18770E+00 
c  Velocity[Z]                                      0.30694E-07 
c  Pressure     0.91783E-10    2237   0.10529E-02   0.13245E+00 0.82983E+03 
c  Void Fractio 0.11334E-08      36   0.41944E-08   0.37319E-02 0.10767E+05 
c  k            0.29592E-03      23   0.29215E-05   0.34798E+00 0.10938E+05 
c  omega        0.86931E+05      15   0.49269E-05   0.73413E+17 0.78195E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -0.00024096                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -3.7          12.754          6.9087           4.187
v  Velocity[Y]            -1.6659          3.2669          -0.112        -0.28902
v  Velocity[Z]         -0.0011682       0.0012057      9.1146e-08      1.8234e-09
v  ǁVelocityǁ            0.028091          12.756          6.9542          4.2052
v  Pressure                1663.3           78371           55994           61565
v  Void Fraction        1.577e-11         0.88738       0.0014676       2.189e-05
v  k                   3.0953e-22          1.7451         0.02261        0.022046
v  omega                   19.613      2.6295e+08      8.3689e+05           70660
v  scalar1                      0               0               0               0
v  TurbVisc            4.0851e-27         0.24329        0.014374         0.12856
v  CourantNb           0.00080305          4.9173         0.86875         0.11952
v  FourierNb            0.0055976         0.85463         0.12664        0.079002
v  total_pressure          1663.3           78371           55994           61565
v  Density Old              112.2            1000          998.63          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016057          5.2218         0.99539         0.19852


 TIME FOR THE TIME STEP               28:        0.16401E+01

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


 INSTANT    0.145000000E-03   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158157465E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18567E+01
   Friction velocity        uet   :  0.96455E-01 0.11442E+01
   Friction velocity        uk    :  0.96443E-01 0.15806E+01
   Dimensionless distance   yplus :  0.23897E+00 0.38189E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        659
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.5562E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43538E-01      22   0.38558E-04   0.48045E+01 0.22112E+03 
c  Velocity[X]                                      0.45803E+01 
c  Velocity[Y]                                      0.22414E+00 
c  Velocity[Z]                                      0.11259E-07 
c  Pressure     0.38298E-08    1499   0.23509E-03   0.10131E+01 0.44293E+03 
c  Void Fractio 0.11526E-08      34   0.53918E-08   0.35734E-02 0.10313E+05 
c  k            0.29590E-03      22   0.61022E-05   0.45022E+00 0.12493E+05 
c  omega        0.87413E+05      16   0.11196E-04   0.95450E+17 0.86769E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.1304e-18                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6916          12.712          6.9029          4.1878
v  Velocity[Y]            -1.6868           3.276        -0.11166         -0.2891
v  Velocity[Z]         -0.0011703       0.0012056       8.976e-08      1.8103e-09
v  ǁVelocityǁ            0.071578          12.713          6.9486           4.206
v  Pressure                1896.7           78101           55764           61453
v  Void Fraction       1.2881e-11          0.8811       0.0015191       2.278e-05
v  k                   4.8785e-22          1.7658        0.021972        0.022034
v  omega                   1.2881      2.4424e+08      8.9705e+05           71497
v  scalar1                      0               0               0               0
v  TurbVisc            6.6183e-27          0.2433        0.014339         0.12848
v  CourantNb           0.00079704          4.8845         0.86816         0.11954
v  FourierNb            0.0056057         0.84669         0.12647        0.078732
v  total_pressure          1896.7           78101           55764           61453
v  Density Old             109.81            1000          998.58          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016063          5.1901         0.99463         0.19827


 TIME FOR THE TIME STEP               29:        0.12797E+01

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


 INSTANT    0.150000000E-03   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158191863E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18566E+01
   Friction velocity        uet   :  0.17134E+00 0.11454E+01
   Friction velocity        uk    :  0.17132E+00 0.15747E+01
   Dimensionless distance   yplus :  0.42434E+00 0.38047E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        706
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.5163E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43549E-01      22   0.40375E-04   0.47034E+01 0.21873E+03 
c  Velocity[X]                                      0.44844E+01 
c  Velocity[Y]                                      0.21898E+00 
c  Velocity[Z]                                      0.17861E-07 
c  Pressure     0.84955E-10    2051   0.14104E-02   0.12036E+00 0.91222E+03 
c  Void Fractio 0.11791E-08      35   0.57711E-08   0.34600E-02 0.99252E+04 
c  k            0.29588E-03      24   0.53517E-05   0.45987E+00 0.12677E+05 
c  omega        0.88747E+05      15   0.77048E-05   0.89449E+17 0.84110E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -5.586e-06                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6483          12.685          6.8972          4.1886
v  Velocity[Y]            -1.7055           3.269        -0.11132        -0.28917
v  Velocity[Z]          -0.001181       0.0012107      8.6802e-08       1.764e-09
v  ǁVelocityǁ            0.020709          12.692           6.943          4.2068
v  Pressure                1897.7           77530           55249           61236
v  Void Fraction       1.0527e-11          0.8738       0.0015726      2.3714e-05
v  k                   7.5036e-22          1.7469        0.021304        0.022022
v  omega                 0.029966      2.4263e+08      9.2899e+05           71455
v  scalar1                      0               0               0               0
v  TurbVisc            1.0431e-26          0.2433        0.014305         0.12839
v  CourantNb           0.00079017          4.8816         0.86757         0.11956
v  FourierNb            0.0056139         0.83951         0.12628        0.078469
v  total_pressure          1897.7           77530           55249           61236
v  Density Old             113.51            1000          998.53          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01607          5.1883         0.99385         0.19803


 TIME FOR THE TIME STEP               30:        0.15607E+01

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


 INSTANT    0.155000000E-03   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158225441E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18573E+01
   Friction velocity        uet   :  0.80728E-01 0.11410E+01
   Friction velocity        uk    :  0.80717E-01 0.15694E+01
   Dimensionless distance   yplus :  0.19992E+00 0.37919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        751
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.4151E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43561E-01      23   0.39716E-04   0.45882E+01 0.21599E+03 
c  Velocity[X]                                      0.43665E+01 
c  Velocity[Y]                                      0.22175E+00 
c  Velocity[Z]                                      0.48027E-07 
c  Pressure     0.69372E-09    2218   0.84255E-03   0.74329E+00 0.95522E+03 
c  Void Fractio 0.12071E-08      36   0.40162E-08   0.37183E-02 0.10058E+05 
c  k            0.29587E-03      24   0.33247E-05   0.41877E+00 0.12142E+05 
c  omega        0.88017E+05      15   0.64704E-05   0.83414E+17 0.81374E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -8.2731e-18                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7775          12.665          6.8914          4.1894
v  Velocity[Y]            -1.7361          3.2382        -0.11099        -0.28925
v  Velocity[Z]         -0.0012396       0.0012025      8.2867e-08      1.6724e-09
v  ǁVelocityǁ            0.058536          12.668          6.9374          4.2076
v  Pressure                1138.3           76972           54723           61002
v  Void Fraction       8.6069e-12         0.86542       0.0016278       2.469e-05
v  k                    1.129e-21          1.7579        0.020658        0.022011
v  omega               0.00084483      2.4138e+08      9.5446e+05           71412
v  scalar1                      0               0               0               0
v  TurbVisc            1.6044e-26          0.2433        0.014271         0.12831
v  CourantNb           0.00078283          4.8896         0.86695         0.11958
v  FourierNb            0.0056222         0.83304         0.12608        0.078213
v  total_pressure          1138.3           76972           54723           61002
v  Density Old             119.78            1000          998.48          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016077          5.1972         0.99304          0.1978


 TIME FOR THE TIME STEP               31:        0.16246E+01

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


 INSTANT    0.160000000E-03   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158258035E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18583E+01
   Friction velocity        uet   :  0.15466E+00 0.11410E+01
   Friction velocity        uk    :  0.15464E+00 0.15646E+01
   Dimensionless distance   yplus :  0.38285E+00 0.37804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        799
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.6808E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43572E-01      22   0.39031E-04   0.46402E+01 0.21717E+03 
c  Velocity[X]                                      0.43440E+01 
c  Velocity[Y]                                      0.29617E+00 
c  Velocity[Z]                                      0.19488E-07 
c  Pressure     0.12421E-07    1528   0.64911E-04   0.10077E+01 0.56867E+03 
c  Void Fractio 0.12403E-08      34   0.53746E-08   0.52081E-02 0.11614E+05 
c  k            0.29586E-03      23   0.34481E-05   0.44303E+00 0.12538E+05 
c  omega        0.87788E+05      14   0.63957E-05   0.85801E+17 0.81980E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.2773e-17                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7782           12.63          6.8855          4.1901
v  Velocity[Y]            -1.7705          3.2298        -0.11062        -0.28932
v  Velocity[Z]         -0.0012491       0.0012297      7.9323e-08      1.5969e-09
v  ǁVelocityǁ            0.021926          12.633          6.9318          4.2084
v  Pressure                1897.9           76630           54404           60866
v  Void Fraction       7.0393e-12         0.86644       0.0016849      2.5707e-05
v  k                    1.665e-21          1.7711        0.019965           0.022
v  omega               2.0924e-05      2.4039e+08      9.9677e+05           71584
v  scalar1                      0               0               0               0
v  TurbVisc             2.414e-26         0.24331        0.014239         0.12823
v  CourantNb           0.00077522           4.853         0.86635          0.1196
v  FourierNb            0.0056303         0.82722         0.12588        0.077964
v  total_pressure          1897.9           76630           54404           60866
v  Density Old             127.07            1000          998.43          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016084          5.1614         0.99223         0.19757


 TIME FOR THE TIME STEP               32:        0.12927E+01

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


 INSTANT    0.165000000E-03   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158290154E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18581E+01
   Friction velocity        uet   :  0.79714E-01 0.11427E+01
   Friction velocity        uk    :  0.79701E-01 0.15599E+01
   Dimensionless distance   yplus :  0.19732E+00 0.37689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        841
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1224E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43583E-01      22   0.38908E-04   0.44301E+01 0.21215E+03 
c  Velocity[X]                                      0.41995E+01 
c  Velocity[Y]                                      0.23059E+00 
c  Velocity[Z]                                      0.14888E-07 
c  Pressure     0.24582E-09    2353   0.13503E-02   0.34068E+00 0.10174E+04 
c  Void Fractio 0.12651E-08      36   0.44426E-08   0.46435E-02 0.10709E+05 
c  k            0.29585E-03      24   0.33397E-05   0.41320E+00 0.12152E+05 
c  omega        0.87885E+05      14   0.60871E-05   0.77478E+17 0.78236E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -0.00015964                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6549          12.609          6.8797          4.1909
v  Velocity[Y]            -1.8178          3.2389        -0.11029        -0.28939
v  Velocity[Z]          -0.001227       0.0012222      7.6713e-08      1.5632e-09
v  ǁVelocityǁ            0.094769          12.611          6.9261          4.2091
v  Pressure                1026.7           76023           53846           60618
v  Void Fraction       5.7601e-12         0.86597       0.0017437      2.6766e-05
v  k                   2.4117e-21          1.7486         0.01928        0.021989
v  omega               1.3864e-06      2.3951e+08      1.0145e+06           71541
v  scalar1                      0               0               0               0
v  TurbVisc            3.5603e-26         0.24331        0.014206         0.12815
v  CourantNb           0.00076725          4.8337         0.86575         0.11962
v  FourierNb            0.0056384           0.822         0.12567         0.07772
v  total_pressure          1026.7           76023           53846           60618
v  Density Old             135.45            1000          998.37          999.98


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016091          5.1431         0.99141         0.19734


 TIME FOR THE TIME STEP               33:        0.16967E+01

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


 INSTANT    0.170000000E-03   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158321185E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18586E+01
   Friction velocity        uet   :  0.19258E+00 0.11451E+01
   Friction velocity        uk    :  0.19255E+00 0.15544E+01
   Dimensionless distance   yplus :  0.47668E+00 0.37557E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        881
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.5737E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43593E-01      22   0.40253E-04   0.45610E+01 0.21522E+03 
c  Velocity[X]                                      0.42492E+01 
c  Velocity[Y]                                      0.31171E+00 
c  Velocity[Z]                                      0.11088E-07 
c  Pressure     0.14812E-07    1404   0.58455E-04   0.10080E+01 0.36052E+03 
c  Void Fractio 0.12983E-08      34   0.49224E-08   0.59333E-02 0.11809E+05 
c  k            0.29584E-03      22   0.32391E-05   0.38126E+00 0.11713E+05 
c  omega        0.88807E+05      14   0.55787E-05   0.73807E+17 0.76360E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -0.00030642                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8583          12.574          6.8739          4.1916
v  Velocity[Y]            -1.8642          3.2297        -0.10993        -0.28946
v  Velocity[Z]         -0.0012058       0.0012019       7.024e-08      1.4343e-09
v  ǁVelocityǁ            0.058818           12.58          6.9204          4.2099
v  Pressure                  1899           75763           53634           60537
v  Void Fraction       4.7144e-12         0.86616       0.0018038      2.7864e-05
v  k                   3.4353e-21          1.7624        0.018643        0.021979
v  omega               3.3595e-07      2.3866e+08      1.0366e+06           71574
v  scalar1                      0               0               0               0
v  TurbVisc            5.1568e-26         0.24331        0.014174         0.12808
v  CourantNb           0.00075936          4.8329          0.8651         0.11964
v  FourierNb            0.0056464         0.81729         0.12546        0.077483
v  total_pressure            1899           75763           53634           60537
v  Density Old             134.43            1000          998.32          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016098           5.143         0.99055         0.19712


 TIME FOR THE TIME STEP               34:        0.12368E+01

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


 INSTANT    0.175000000E-03   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158352017E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18588E+01
   Friction velocity        uet   :  0.15559E+00 0.11268E+01
   Friction velocity        uk    :  0.15557E+00 0.15511E+01
   Dimensionless distance   yplus :  0.38506E+00 0.37478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        910
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.7175E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43604E-01      23   0.39776E-04   0.42391E+01 0.20745E+03 
c  Velocity[X]                                      0.39982E+01 
c  Velocity[Y]                                      0.24091E+00 
c  Velocity[Z]                                      0.20642E-07 
c  Pressure     0.10791E-09    2105   0.13941E-02   0.15399E+00 0.90109E+03 
c  Void Fractio 0.13342E-08      37   0.39924E-08   0.63096E-02 0.11881E+05 
c  k            0.29582E-03      23   0.51914E-05   0.32090E+00 0.10777E+05 
c  omega        0.87615E+05      13   0.82422E-05   0.58759E+17 0.68950E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -4.0566e-17                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9905          12.554          6.8683          4.1923
v  Velocity[Y]            -1.9091          3.2108         -0.1096        -0.28953
v  Velocity[Z]         -0.0011878       0.0011831      7.3108e-08      1.4911e-09
v  ǁVelocityǁ            0.015247          12.556          6.9149          4.2106
v  Pressure                1109.6           75243           53146           60315
v  Void Fraction       3.8603e-12          0.8687       0.0018657      2.9002e-05
v  k                   4.8188e-21          1.7513        0.018095        0.021969
v  omega               6.1098e-05      2.3637e+08       1.018e+06           71540
v  scalar1                      0               0               0               0
v  TurbVisc            7.3457e-26         0.24332        0.014143           0.128
v  CourantNb           0.00075126           4.809         0.86446         0.11966
v  FourierNb            0.0056543           0.817         0.12524        0.077251
v  total_pressure          1109.6           75243           53146           60315
v  Density Old              134.9            1000          998.26          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016104          5.1199          0.9897         0.19691


 TIME FOR THE TIME STEP               35:        0.15896E+01

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


 INSTANT    0.180000000E-03   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158381826E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18593E+01
   Friction velocity        uet   :  0.64576E-01 0.11446E+01
   Friction velocity        uk    :  0.64566E-01 0.15479E+01
   Dimensionless distance   yplus :  0.15981E+00 0.37401E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        927
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1634E-11


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43614E-01      22   0.41472E-04   0.41322E+01 0.20478E+03 
c  Velocity[X]                                      0.37990E+01 
c  Velocity[Y]                                      0.33316E+00 
c  Velocity[Z]                                      0.11920E-07 
c  Pressure     0.13336E-07    1316   0.80005E-04   0.10084E+01 0.16272E+03 
c  Void Fractio 0.13696E-08      35   0.61666E-08   0.62975E-02 0.11565E+05 
c  k            0.29582E-03      21   0.50327E-05   0.20931E+00 0.87208E+04 
c  omega        0.87705E+05      14   0.52423E-05   0.38284E+17 0.56725E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -1.386e-05                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0172           12.53          6.8628           4.193
v  Velocity[Y]            -1.9541          3.2138        -0.10926         -0.2896
v  Velocity[Z]         -0.0011778       0.0011657      7.2036e-08      1.4664e-09
v  ǁVelocityǁ            0.043726          12.532          6.9097          4.2113
v  Pressure                1899.8           75031           53044           60298
v  Void Fraction       3.1614e-12         0.87108       0.0019291      3.0178e-05
v  k                   6.6653e-21          1.7329        0.017726        0.021961
v  omega               1.9689e-06      2.1065e+08       9.913e+05           70910
v  scalar1                      0               0               0               0
v  TurbVisc            1.0304e-25         0.24332        0.014113         0.12793
v  CourantNb           0.00074341          4.7931          0.8638         0.11967
v  FourierNb            0.0056622         0.81644         0.12506        0.077025
v  total_pressure          1899.8           75031           53044           60298
v  Density Old              134.7            1000           998.2          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016111          5.1045         0.98886          0.1967


 TIME FOR THE TIME STEP               36:        0.12177E+01

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


 INSTANT    0.185000000E-03   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158411805E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18590E+01
   Friction velocity        uet   :  0.13400E+00 0.11291E+01
   Friction velocity        uk    :  0.13398E+00 0.15439E+01
   Dimensionless distance   yplus :  0.33159E+00 0.37303E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        943
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.9375E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43624E-01      23   0.41589E-04   0.39433E+01 0.20000E+03 
c  Velocity[X]                                      0.36771E+01 
c  Velocity[Y]                                      0.26614E+00 
c  Velocity[Z]                                      0.55797E-07 
c  Pressure     0.37909E-09    1991   0.12927E-02   0.50681E+00 0.71925E+03 
c  Void Fractio 0.13993E-08      35   0.56601E-08   0.61408E-02 0.11147E+05 
c  k            0.29581E-03      23   0.23389E-05   0.16208E+00 0.76862E+04 
c  omega        0.86821E+05      14   0.32264E-05   0.29621E+17 0.50275E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -7.9376e-17                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.92          12.506          6.8574          4.1937
v  Velocity[Y]              -2.01          3.2142        -0.10896        -0.28967
v  Velocity[Z]         -0.0011843       0.0009707      6.4772e-08      1.2951e-09
v  ǁVelocityǁ            0.018087          12.509          6.9045           4.212
v  Pressure                1170.2           74618           52640           60129
v  Void Fraction         2.59e-12         0.87429       0.0019942      3.1393e-05
v  k                   9.1003e-21          1.7096         0.01744        0.021955
v  omega               9.1295e-08      2.0099e+08      9.8417e+05           70577
v  scalar1                      0               0               0               0
v  TurbVisc            1.4252e-25         0.24332        0.014083         0.12786
v  CourantNb           0.00073533          4.7684         0.86319         0.11969
v  FourierNb            0.0056699          0.8153          0.1249        0.076804
v  total_pressure          1170.2           74618           52640           60129
v  Density Old             132.17            1000          998.14          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016118          5.0807         0.98809          0.1965


 TIME FOR THE TIME STEP               37:        0.15505E+01

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


 INSTANT    0.190000000E-03   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158441092E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18596E+01
   Friction velocity        uet   :  0.76717E-01 0.11208E+01
   Friction velocity        uk    :  0.76705E-01 0.15395E+01
   Dimensionless distance   yplus :  0.18984E+00 0.37196E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        959
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.6544E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43634E-01      22   0.41881E-04   0.40792E+01 0.20339E+03 
c  Velocity[X]                                      0.37314E+01 
c  Velocity[Y]                                      0.34782E+00 
c  Velocity[Z]                                      0.40018E-07 
c  Pressure     0.12590E-07    1361   0.81846E-04   0.10098E+01 0.30466E+03 
c  Void Fractio 0.14383E-08      34   0.56717E-08   0.62730E-02 0.10981E+05 
c  k            0.29581E-03      23   0.22645E-05   0.15653E+00 0.75650E+04 
c  omega        0.86567E+05      15   0.27582E-05   0.28376E+17 0.49192E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.0842e-16                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.984          12.485          6.8522          4.1944
v  Velocity[Y]            -2.0362          3.1993        -0.10865        -0.28973
v  Velocity[Z]          -0.001479       0.0012438      6.5559e-08      1.2644e-09
v  ǁVelocityǁ            0.071667          12.486          6.8994          4.2127
v  Pressure                1901.2           74381           52458           60065
v  Void Fraction       2.1224e-12         0.87505       0.0020604      3.2645e-05
v  k                   1.2276e-20          1.7027        0.017175        0.021949
v  omega               8.6468e-08      2.0102e+08      9.9022e+05           70480
v  scalar1                      0               0               0               0
v  TurbVisc            1.9459e-25         0.24333        0.014055         0.12779
v  CourantNb           0.00072759          4.7753          0.8626         0.11971
v  FourierNb            0.0056775         0.81307         0.12475        0.076589
v  total_pressure          1901.2           74381           52458           60065
v  Density Old             129.79            1000          998.07          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016124          5.0884         0.98735          0.1963


 TIME FOR THE TIME STEP               38:        0.12411E+01

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


 INSTANT    0.195000000E-03   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158470246E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18604E+01
   Friction velocity        uet   :  0.16105E+00 0.11480E+01
   Friction velocity        uk    :  0.16101E+00 0.15365E+01
   Dimensionless distance   yplus :  0.39767E+00 0.37124E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        974
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.5775E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43644E-01      23   0.43407E-04   0.37709E+01 0.19551E+03 
c  Velocity[X]                                      0.34874E+01 
c  Velocity[Y]                                      0.28350E+00 
c  Velocity[Z]                                      0.23088E-07 
c  Pressure     0.11291E-09    2221   0.15867E-02   0.16614E+00 0.62721E+03 
c  Void Fractio 0.14759E-08      36   0.50274E-08   0.65210E-02 0.10922E+05 
c  k            0.29580E-03      24   0.25812E-05   0.14982E+00 0.74116E+04 
c  omega        0.86592E+05      14   0.38327E-05   0.26510E+17 0.47569E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.4605e-16                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1235          12.462          6.8471          4.1951
v  Velocity[Y]            -2.0687          3.1778        -0.10836         -0.2898
v  Velocity[Z]         -0.0014561       0.0014788      6.7911e-08      1.3009e-09
v  ǁVelocityǁ            0.016122          12.463          6.8944          4.2134
v  Pressure                1354.8           74016           52112           59914
v  Void Fraction       1.7397e-12         0.87506       0.0021282      3.3935e-05
v  k                   1.6374e-20          1.7251        0.016927        0.021944
v  omega               2.0284e-08      2.0502e+08      9.9664e+05           70420
v  scalar1                      0               0               0               0
v  TurbVisc            2.6249e-25         0.24333        0.014026         0.12772
v  CourantNb           0.00071956          4.7609         0.86202         0.11973
v  FourierNb            0.0056851         0.80894          0.1246        0.076378
v  total_pressure          1354.8           74016           52112           59914
v  Density Old             126.59            1000          998.01          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016131          5.0746         0.98663          0.1961


 TIME FOR THE TIME STEP               39:        0.16544E+01

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


 INSTANT    0.200000000E-03   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158498768E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18608E+01
   Friction velocity        uet   :  0.80167E-01 0.11333E+01
   Friction velocity        uk    :  0.80155E-01 0.15332E+01
   Dimensionless distance   yplus :  0.19839E+00 0.37044E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        987
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.9295E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43654E-01      23   0.41711E-04   0.38809E+01 0.19831E+03 
c  Velocity[X]                                      0.35239E+01 
c  Velocity[Y]                                      0.35700E+00 
c  Velocity[Z]                                      0.24610E-07 
c  Pressure     0.91829E-08    1508   0.10888E-03   0.10124E+01 0.30965E+03 
c  Void Fractio 0.15160E-08      36   0.45340E-08   0.73898E-02 0.11337E+05 
c  k            0.29580E-03      22   0.21046E-05   0.14103E+00 0.72010E+04 
c  omega        0.86561E+05      13   0.20282E-05   0.23775E+17 0.45116E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.9421e-16                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1968          12.433           6.842          4.1957
v  Velocity[Y]             -2.092          3.1816        -0.10807        -0.28987
v  Velocity[Z]         -0.0013314       0.0016239      6.5086e-08      1.2341e-09
v  ǁVelocityǁ            0.042729          12.435          6.8896           4.214
v  Pressure                1901.6           73766           51934           59844
v  Void Fraction       1.4263e-12         0.87617       0.0021972      3.5262e-05
v  k                    2.161e-20          1.7175        0.016692        0.021939
v  omega               6.5516e-09      2.0104e+08      1.0003e+06           70321
v  scalar1                      0               0               0               0
v  TurbVisc            3.5012e-25         0.24333        0.013999         0.12765
v  CourantNb           0.00071172          4.7378         0.86146         0.11974
v  FourierNb            0.0056926         0.80216         0.12446        0.076171
v  total_pressure          1901.6           73766           51934           59844
v  Density Old             125.82            1000          997.94          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016138          5.0519         0.98593         0.19591


 TIME FOR THE TIME STEP               40:        0.13290E+01

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


 INSTANT    0.205000000E-03   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158527145E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18606E+01
   Friction velocity        uet   :  0.12798E+00 0.11258E+01
   Friction velocity        uk    :  0.12796E+00 0.15295E+01
   Dimensionless distance   yplus :  0.31669E+00 0.36954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.9865E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43664E-01      23   0.42669E-04   0.35792E+01 0.19041E+03 
c  Velocity[X]                                      0.32558E+01 
c  Velocity[Y]                                      0.32336E+00 
c  Velocity[Z]                                      0.11403E-07 
c  Pressure     0.32935E-09    2228   0.14983E-02   0.46115E+00 0.60015E+03 
c  Void Fractio 0.15574E-08      35   0.61094E-08   0.69337E-02 0.10713E+05 
c  k            0.29580E-03      23   0.18194E-05   0.12291E+00 0.67305E+04 
c  omega        0.86501E+05      14   0.23647E-05   0.21742E+17 0.43183E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.5521e-16                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1472          12.425          6.8371          4.1964
v  Velocity[Y]            -2.1308          3.1864        -0.10778        -0.28993
v  Velocity[Z]         -0.0013608       0.0017279      6.0324e-08       1.131e-09
v  ǁVelocityǁ            0.019903          12.425          6.8848          4.2147
v  Pressure                1550.5           73415           51605           59701
v  Void Fraction       1.1697e-12         0.88103       0.0022678      3.6625e-05
v  k                   2.8242e-20          1.6999        0.016481        0.021934
v  omega                 2.78e-09      2.0098e+08      1.0055e+06           70244
v  scalar1                      0               0               0               0
v  TurbVisc            4.6207e-25         0.24334        0.013972         0.12759
v  CourantNb           0.00070398          4.7231         0.86091         0.11976
v  FourierNb            0.0056996         0.79465         0.12433        0.075968
v  total_pressure          1550.5           73415           51605           59701
v  Density Old             125.81            1000          997.87          999.97


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016143          5.0314         0.98524         0.19573


 TIME FOR THE TIME STEP               41:        0.16603E+01

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


 INSTANT    0.210000000E-03   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158554915E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18606E+01
   Friction velocity        uet   :  0.89513E-01 0.11259E+01
   Friction velocity        uk    :  0.89500E-01 0.15267E+01
   Dimensionless distance   yplus :  0.22155E+00 0.36888E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.4747E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43673E-01      24   0.42215E-04   0.38036E+01 0.19626E+03 
c  Velocity[X]                                      0.34474E+01 
c  Velocity[Y]                                      0.35621E+00 
c  Velocity[Z]                                      0.13259E-07 
c  Pressure     0.60220E-08    1566   0.16916E-03   0.10177E+01 0.30174E+03 
c  Void Fractio 0.15952E-08      36   0.51681E-08   0.76004E-02 0.10942E+05 
c  k            0.29579E-03      24   0.20153E-05   0.13087E+00 0.69540E+04 
c  omega        0.86443E+05      13   0.18170E-05   0.23027E+17 0.44320E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -3.224e-16                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1406          12.399          6.8322           4.197
v  Velocity[Y]            -2.1589          3.1819         -0.1075           -0.29
v  Velocity[Z]         -0.0013537       0.0018209      5.5595e-08      1.0402e-09
v  ǁVelocityǁ            0.036479            12.4          6.8801          4.2153
v  Pressure                1902.7           73175           51430           59634
v  Void Fraction       9.5943e-13         0.88353       0.0023397      3.8024e-05
v  k                   3.6574e-20           1.677        0.016271        0.021929
v  omega               2.9821e-09      2.0094e+08      1.0164e+06           70263
v  scalar1                      0               0               0               0
v  TurbVisc            6.0388e-25         0.24334        0.013945         0.12752
v  CourantNb           0.00069645          4.7266         0.86038         0.11978
v  FourierNb            0.0057064          0.7904         0.12421         0.07577
v  total_pressure          1902.7           73175           51430           59634
v  Density Old              124.7            1000          997.81          999.96


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016149          5.0302         0.98459         0.19555


 TIME FOR THE TIME STEP               42:        0.13449E+01

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


 INSTANT    0.215000000E-03   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158582490E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18608E+01
   Friction velocity        uet   :  0.11762E+00 0.11259E+01
   Friction velocity        uk    :  0.11760E+00 0.15237E+01
   Dimensionless distance   yplus :  0.29110E+00 0.36816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1489E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43683E-01      23   0.40351E-04   0.35740E+01 0.19021E+03 
c  Velocity[X]                                      0.32335E+01 
c  Velocity[Y]                                      0.34047E+00 
c  Velocity[Z]                                      0.15583E-07 
c  Pressure     0.10859E-09    1994   0.16553E-02   0.16376E+00 0.75865E+03 
c  Void Fractio 0.16400E-08      36   0.62923E-08   0.79733E-02 0.10936E+05 
c  k            0.29579E-03      23   0.19325E-05   0.12806E+00 0.68873E+04 
c  omega        0.86510E+05      13   0.21535E-05   0.22454E+17 0.43733E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -4.1655e-16                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0577          12.387          6.8274          4.1977
v  Velocity[Y]            -2.1913          3.1471        -0.10721        -0.29007
v  Velocity[Z]         -0.0014136       0.0018936      5.6892e-08      1.0793e-09
v  ǁVelocityǁ            0.027475          12.387          6.8754           4.216
v  Pressure                1802.5           72677           51018           59454
v  Void Fraction       7.8726e-13          0.8869       0.0024129      3.9458e-05
v  k                    4.696e-20          1.6873        0.016061        0.021925
v  omega               7.9131e-09      2.0085e+08      1.0246e+06           70274
v  scalar1                      0               0               0               0
v  TurbVisc            7.8204e-25         0.24334        0.013919         0.12746
v  CourantNb           0.00068914          4.7127         0.85983         0.11979
v  FourierNb            0.0057132         0.79578         0.12408        0.075576
v  total_pressure          1802.5           72677           51018           59454
v  Density Old             119.85            1000          997.73          999.96


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016155          5.0282         0.98391         0.19537


 TIME FOR THE TIME STEP               43:        0.15494E+01

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


 INSTANT    0.220000000E-03   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158609267E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18608E+01
   Friction velocity        uet   :  0.10619E+00 0.11278E+01
   Friction velocity        uk    :  0.10618E+00 0.15199E+01
   Dimensionless distance   yplus :  0.26289E+00 0.36723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.5702E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43692E-01      23   0.41940E-04   0.35805E+01 0.19035E+03 
c  Velocity[X]                                      0.32193E+01 
c  Velocity[Y]                                      0.36121E+00 
c  Velocity[Z]                                      0.22753E-07 
c  Pressure     0.20310E-08    1739   0.51669E-03   0.10109E+01 0.34811E+03 
c  Void Fractio 0.16816E-08      36   0.61397E-08   0.80244E-02 0.10707E+05 
c  k            0.29579E-03      23   0.19981E-05   0.13294E+00 0.70263E+04 
c  omega        0.24811E+08      34   0.16455E-02   0.78192E+27 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -5.1928e-16                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1749          12.368          6.8226          4.1983
v  Velocity[Y]            -2.2313          3.1459        -0.10694        -0.29013
v  Velocity[Z]         -0.0014576       0.0019435      5.4745e-08       1.025e-09
v  ǁVelocityǁ            0.028961          12.369          6.8708          4.2166
v  Pressure                1902.8           72473           50823           59374
v  Void Fraction       6.4611e-13         0.89634       0.0024873      4.0927e-05
v  k                   5.9812e-20          1.6766        0.015847         0.02192
v  omega               2.0395e-05      1.2033e+14       3.024e+09      4.4294e+07
v  scalar1                      0               0               0               0
v  TurbVisc            1.0041e-24         0.24335        0.013894          0.1274
v  CourantNb           0.00068205          4.6963         0.85931         0.11981
v  FourierNb            0.0057199         0.81786         0.12395        0.075386
v  total_pressure          1902.8           72473           50823           59374
v  Density Old             117.35            1000          997.66          999.96


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01616          5.0068         0.98326         0.19519


 TIME FOR THE TIME STEP               44:        0.14178E+01

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


 INSTANT    0.225000000E-03   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158635762E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18605E+01
   Friction velocity        uet   :  0.10374E+00 0.11294E+01
   Friction velocity        uk    :  0.10373E+00 0.15172E+01
   Dimensionless distance   yplus :  0.25682E+00 0.36657E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1051
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1463E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43701E-01      23   0.40959E-04   0.35125E+01 0.18850E+03 
c  Velocity[X]                                      0.31532E+01 
c  Velocity[Y]                                      0.35931E+00 
c  Velocity[Z]                                      0.25304E-07 
c  Pressure     0.10706E-09    2029   0.15788E-02   0.16216E+00 0.69504E+03 
c  Void Fractio 0.17262E-08      36   0.59930E-08   0.83829E-02 0.10686E+05 
c  k            0.29579E-03      21   0.19523E-05   0.13884E+00 0.71901E+04 
c  omega        0.69803E+15       2   0.29795E-10   0.19548E+27 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.2135e-10                             6
a  omega             -5.1964e+05                             3
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1921          12.343          6.8179          4.1989
v  Velocity[Y]             -2.244          3.1569        -0.10665        -0.29019
v  Velocity[Z]         -0.0014969       0.0019929      5.3528e-08      9.8931e-10
v  ǁVelocityǁ            0.035303          12.344          6.8663          4.2172
v  Pressure                1903.8           72024           50448           59209
v  Void Fraction       5.3045e-13         0.90501       0.0025629      4.2429e-05
v  k                   7.5606e-20          1.6546        0.015567        0.021915
v  omega               3.4791e-06      6.0163e+13      1.5127e+09      2.2186e+07
v  scalar1                      0               0               0               0
v  TurbVisc            1.2789e-24         0.24335        0.013869         0.12733
v  CourantNb           0.00067512          4.6844         0.85878         0.11982
v  FourierNb            0.0057267         0.83092         0.12381        0.075198
v  total_pressure          1903.8           72024           50448           59209
v  Density Old             113.99            1000          997.59          999.96


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016166          4.9789         0.98259         0.19502


 TIME FOR THE TIME STEP               45:        0.15811E+01

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


 INSTANT    0.230000000E-03   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158661529E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18599E+01
   Friction velocity        uet   :  0.11533E+00 0.11315E+01
   Friction velocity        uk    :  0.11533E+00 0.15154E+01
   Dimensionless distance   yplus :  0.28832E+00 0.36615E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1067
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1200E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43709E-01      23   0.40763E-04   0.35718E+01 0.19006E+03 
c  Velocity[X]                                      0.31887E+01 
c  Velocity[Y]                                      0.38308E+00 
c  Velocity[Z]                                      0.10153E-07 
c  Pressure     0.38073E-09    1913   0.14116E-02   0.53157E+00 0.50343E+03 
c  Void Fractio 0.17699E-08      37   0.49991E-08   0.90134E-02 0.10825E+05 
c  k            0.29578E-03      21   0.20123E-05   0.14809E+00 0.74361E+04 
c  omega        0.17070E+15       2   0.61120E-10   0.48870E+26 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.0096e-07                            11
a  omega              -1.111e+07                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1728          12.328          6.8132          4.1995
v  Velocity[Y]            -2.2811          3.1527        -0.10637        -0.29025
v  Velocity[Z]         -0.0015001       0.0020134      5.1409e-08      9.2216e-10
v  ǁVelocityǁ            0.022558          12.328          6.8618          4.2178
v  Pressure                1904.3           71724           50174           59091
v  Void Fraction       4.3561e-13         0.90989       0.0026397      4.3964e-05
v  k                   9.4853e-20          1.6425        0.015334         0.02191
v  omega               3.8987e-07      3.0081e+13      7.5692e+08      1.1128e+07
v  scalar1                      0               0               0               0
v  TurbVisc            6.3849e-25         0.24335        0.013846         0.12728
v  CourantNb           0.00066838          4.6937         0.85826         0.11984
v  FourierNb            0.0057336         0.83447         0.12371        0.075019
v  total_pressure          1904.3           71724           50174           59091
v  Density Old             104.56            1000          997.52          999.96


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016171          4.9801         0.98198         0.19486


 TIME FOR THE TIME STEP               46:        0.14934E+01

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


 INSTANT    0.235000000E-03   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158686803E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18599E+01
   Friction velocity        uet   :  0.89618E-01 0.11353E+01
   Friction velocity        uk    :  0.89605E-01 0.15122E+01
   Dimensionless distance   yplus :  0.22191E+00 0.36537E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1094
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1271E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43718E-01      23   0.42390E-04   0.36202E+01 0.19131E+03 
c  Velocity[X]                                      0.32377E+01 
c  Velocity[Y]                                      0.38250E+00 
c  Velocity[Z]                                      0.29574E-07 
c  Pressure     0.26928E-09    1896   0.17210E-02   0.39321E+00 0.59739E+03 
c  Void Fractio 0.18144E-08      37   0.44956E-08   0.87475E-02 0.10421E+05 
c  k            0.29577E-03      21   0.21550E-05   0.26886E+00 0.10045E+05 
c  omega        0.41555E+14       3   0.12550E-09   0.12218E+26 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.0879e-06                            17
a  omega             -4.4124e+06                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.112          12.306          6.8084          4.2001
v  Velocity[Y]            -2.3054          3.1351        -0.10607        -0.29032
v  Velocity[Z]          -0.001441       0.0020485      5.6592e-08      1.0312e-09
v  ǁVelocityǁ            0.030744          12.306          6.8572          4.2184
v  Pressure                1904.9           71432           49860           58947
v  Void Fraction        3.578e-13         0.91346       0.0027177      4.5531e-05
v  k                    1.182e-19          1.6274        0.015006        0.021904
v  omega               1.1364e-07      1.5041e+13      3.7906e+08      5.6006e+06
v  scalar1                      0               0               0               0
v  TurbVisc            3.5467e-30         0.24336        0.013823         0.12722
v  CourantNb           0.00066189          4.6923         0.85775         0.11985
v  FourierNb            0.0057405         0.83211         0.12361        0.074843
v  total_pressure          1904.9           71432           49860           58947
v  Density Old             95.897            1000          997.44          999.96


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016177          4.9829         0.98136          0.1947


 TIME FOR THE TIME STEP               47:        0.14904E+01

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


 INSTANT    0.240000000E-03   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158711414E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18596E+01
   Friction velocity        uet   :  0.99306E-01 0.11384E+01
   Friction velocity        uk    :  0.99306E-01 0.15075E+01
   Dimensionless distance   yplus :  0.24690E+00 0.36424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1095
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1387E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43727E-01      23   0.41067E-04   0.34016E+01 0.18541E+03 
c  Velocity[X]                                      0.30241E+01 
c  Velocity[Y]                                      0.37750E+00 
c  Velocity[Z]                                      0.11412E-07 
c  Pressure     0.54032E-09    1968   0.14115E-02   0.68379E+00 0.63094E+03 
c  Void Fractio 0.18580E-08      38   0.45070E-08   0.87009E-02 0.10164E+05 
c  k            0.29577E-03      21   0.21656E-05   0.10745E+00 0.63557E+04 
c  omega        0.10074E+14       3   0.25687E-09   0.30544E+25 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.1609e-06                            18
a  omega             -4.4472e+05                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0042          12.278          6.8038          4.2006
v  Velocity[Y]            -2.3408          3.1281        -0.10578        -0.29038
v  Velocity[Z]         -0.0014979       0.0020929      6.2868e-08       1.181e-09
v  ǁVelocityǁ             0.02078          12.279          6.8529           4.219
v  Pressure                1630.2           71002           49520           58801
v  Void Fraction       2.9399e-13         0.91769       0.0027968      4.7129e-05
v  k                   1.4636e-19          1.6039        0.014777        0.021899
v  omega               2.1661e-08      7.5204e+12      1.9004e+08      2.8352e+06
v  scalar1                      0               0               0               0
v  TurbVisc            5.1943e-29         0.24336        0.013799         0.12716
v  CourantNb           0.00065559          4.6709         0.85722         0.11987
v  FourierNb            0.0057474         0.82621         0.12346        0.074664
v  total_pressure          1630.2           71002           49520           58801
v  Density Old             91.018            1000          997.36          999.96


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016182          4.9642         0.98067         0.19453


 TIME FOR THE TIME STEP               48:        0.15198E+01

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


 INSTANT    0.245000000E-03   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158735399E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18596E+01
   Friction velocity        uet   :  0.84851E-01 0.11401E+01
   Friction velocity        uk    :  0.84839E-01 0.15068E+01
   Dimensionless distance   yplus :  0.21014E+00 0.36407E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1097
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.4003E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43735E-01      23   0.40366E-04   0.33538E+01 0.18408E+03 
c  Velocity[X]                                      0.29439E+01 
c  Velocity[Y]                                      0.40996E+00 
c  Velocity[Z]                                      0.56428E-07 
c  Pressure     0.45660E-08    1586   0.25523E-03   0.10198E+01 0.44464E+03 
c  Void Fractio 0.19010E-08      37   0.58377E-08   0.89667E-02 0.10093E+05 
c  k            0.29577E-03      21   0.21831E-05   0.22960E-01 0.29388E+04 
c  omega        0.24469E+13       3   0.52181E-09   0.76359E+24 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.6522e-06                            19
a  omega             -1.2273e+06                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0778          12.262          6.7993          4.2012
v  Velocity[Y]            -2.3619          3.1209         -0.1055        -0.29043
v  Velocity[Z]         -0.0014839       0.0020173      7.6136e-08      1.4795e-09
v  ǁVelocityǁ            0.026044          12.262          6.8486          4.2196
v  Pressure                1905.1           70636           49277           58703
v  Void Fraction       2.4163e-13         0.92481       0.0028768      4.8758e-05
v  k                   1.8015e-19          1.6176        0.014706        0.021896
v  omega               3.4232e-09      3.7602e+12      9.5543e+07      1.4526e+06
v  scalar1                      0               0               0               0
v  TurbVisc            1.6109e-28         0.24336        0.013776          0.1271
v  CourantNb            0.0006495          4.6419         0.85673         0.11988
v  FourierNb            0.0057544         0.82162         0.12336        0.074489
v  total_pressure          1905.1           70636           49277           58703
v  Density Old             87.448            1000          997.29          999.95


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016188          4.9387         0.98008         0.19437


 TIME FOR THE TIME STEP               49:        0.13659E+01

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


 INSTANT    0.250000000E-03   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158759016E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18594E+01
   Friction velocity        uet   :  0.88733E-01 0.11432E+01
   Friction velocity        uk    :  0.88733E-01 0.15025E+01
   Dimensionless distance   yplus :  0.22183E+00 0.36304E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1098
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1151E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43743E-01      23   0.39603E-04   0.31026E+01 0.17703E+03 
c  Velocity[X]                                      0.27234E+01 
c  Velocity[Y]                                      0.37928E+00 
c  Velocity[Z]                                      0.23785E-07 
c  Pressure     0.10628E-09    2102   0.17145E-02   0.16543E+00 0.73237E+03 
c  Void Fractio 0.19471E-08      38   0.45345E-08   0.89462E-02 0.98670E+04 
c  k            0.29577E-03      21   0.22073E-05   0.21927E-01 0.28727E+04 
c  omega        0.59660E+12       3   0.10519E-08   0.19090E+24 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.3913e-06                            20
a  omega                  -27193                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0743          12.225          6.7949          4.2017
v  Velocity[Y]            -2.3744          3.1311        -0.10522        -0.29049
v  Velocity[Z]         -0.0015074        0.001867      8.4804e-08      1.6667e-09
v  ǁVelocityǁ            0.011632          12.228          6.8444          4.2201
v  Pressure                1745.4           70176           48888           58532
v  Void Fraction       1.9867e-13         0.92735       0.0029577      5.0417e-05
v  k                   2.2048e-19          1.6027        0.014651        0.021894
v  omega               5.0076e-10      1.8801e+12      4.8294e+07       7.613e+05
v  scalar1                      0               0               0               0
v  TurbVisc            5.7212e-27         0.24337        0.013754         0.12705
v  CourantNb           0.00064345          4.6527         0.85624          0.1199
v  FourierNb            0.0057614         0.81792         0.12327        0.074318
v  total_pressure          1745.4           70176           48888           58532
v  Density Old             83.227            1000          997.21          999.95


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016194          4.9411         0.97951         0.19421


 TIME FOR THE TIME STEP               50:        0.17350E+01

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


 INSTANT    0.255000000E-03   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158781868E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18594E+01
   Friction velocity        uet   :  0.52411E-01 0.11468E+01
   Friction velocity        uk    :  0.52404E-01 0.14976E+01
   Dimensionless distance   yplus :  0.12981E+00 0.36183E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1100
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1682E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43751E-01      23   0.39802E-04   0.31789E+01 0.17916E+03 
c  Velocity[X]                                      0.27766E+01 
c  Velocity[Y]                                      0.40220E+00 
c  Velocity[Z]                                      0.20037E-07 
c  Pressure     0.31029E-08    1625   0.37051E-03   0.10206E+01 0.51449E+03 
c  Void Fractio 0.19905E-08      38   0.51210E-08   0.94400E-02 0.99249E+04 
c  k            0.29578E-03      22   0.20714E-05   0.17699E-01 0.25816E+04 
c  omega        0.14610E+12       3   0.21042E-08   0.47725E+23 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.2207e-06                            16
a  omega             -1.3711e+06                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0388          12.203          6.7905          4.2022
v  Velocity[Y]            -2.4024          3.1166        -0.10495        -0.29055
v  Velocity[Z]         -0.0014885       0.0018533      8.3668e-08      1.6285e-09
v  ǁVelocityǁ            0.019753          12.205          6.8403          4.2206
v  Pressure                1905.3           69815           48611           58415
v  Void Fraction        1.634e-13         0.92792       0.0030395      5.2105e-05
v  k                   2.6848e-19          1.5899        0.014612        0.021892
v  omega               8.0726e-11      9.4005e+11      2.4672e+07      4.1565e+05
v  scalar1                      0               0               0               0
v  TurbVisc            4.2679e-26         0.24337        0.013732         0.12699
v  CourantNb           0.00063768          4.6708         0.85579         0.11991
v  FourierNb            0.0057685         0.81472         0.12319        0.074149
v  total_pressure          1905.3           69815           48611           58415
v  Density Old              76.12            1000          997.13          999.95


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016199          4.9598         0.97898         0.19406


 TIME FOR THE TIME STEP               51:        0.13683E+01

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


 INSTANT    0.260000000E-03   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158804239E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18727E+01
   Friction velocity        uet   :  0.67838E-01 0.10014E+01
   Friction velocity        uk    :  0.67838E-01 0.14940E+01
   Dimensionless distance   yplus :  0.16960E+00 0.36098E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1100
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1284E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43759E-01      23   0.38759E-04   0.29917E+01 0.17378E+03 
c  Velocity[X]                                      0.25995E+01 
c  Velocity[Y]                                      0.39227E+00 
c  Velocity[Z]                                      0.76687E-08 
c  Pressure     0.13580E-09    1958   0.17922E-02   0.21251E+00 0.68473E+03 
c  Void Fractio 0.20341E-08      39   0.43733E-08   0.97339E-02 0.98744E+04 
c  k            0.29578E-03      22   0.11219E-05   0.71575E-02 0.16420E+04 
c  omega        0.35926E+11       3   0.41897E-08   0.11931E+23 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.1099e-06                            14
a  omega             -2.1731e+07                             3
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.024           12.17          6.7863          4.2028
v  Velocity[Y]              -2.43          3.1121        -0.10467         -0.2906
v  Velocity[Z]         -0.0015372        0.001833      8.7483e-08      1.7062e-09
v  ǁVelocityǁ           0.0094507          12.171          6.8363          4.2212
v  Pressure                1795.3           69365           48251           58255
v  Void Fraction       1.3443e-13         0.93136       0.0031222      5.3822e-05
v  k                   3.2523e-19          1.5931        0.014584        0.021891
v  omega               1.3008e-11      4.7002e+11      1.2858e+07      2.4272e+05
v  scalar1                      0               0               0               0
v  TurbVisc            2.5427e-25         0.24337        0.013711         0.12694
v  CourantNb           0.00063204          4.6744         0.85533         0.11993
v  FourierNb            0.0057757         0.81194          0.1231        0.073983
v  total_pressure          1795.3           69365           48251           58255
v  Density Old             73.574            1000          997.05          999.95


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016205          4.9637         0.97844         0.19391


 TIME FOR THE TIME STEP               52:        0.15459E+01

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


 INSTANT    0.265000000E-03   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158825879E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18774E+01
   Friction velocity        uet   :  0.31774E-01 0.11129E+01
   Friction velocity        uk    :  0.31774E-01 0.14909E+01
   Dimensionless distance   yplus :  0.78626E-01 0.36023E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1102
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2046E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43766E-01      23   0.39735E-04   0.30961E+01 0.17677E+03 
c  Velocity[X]                                      0.26979E+01 
c  Velocity[Y]                                      0.39824E+00 
c  Velocity[Z]                                      0.35716E-07 
c  Pressure     0.23574E-08    1823   0.50652E-03   0.10161E+01 0.46843E+03 
c  Void Fractio 0.20766E-08      38   0.58286E-08   0.97508E-02 0.96863E+04 
c  k            0.29578E-03      21   0.12175E-05   0.73482E-02 0.16639E+04 
c  omega        0.30989E+13       2   0.23952E-10   0.29828E+22 0.19998E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -9.2465e-07                            14
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0057          12.139           6.782          4.2033
v  Velocity[Y]            -2.4505          3.1008        -0.10441        -0.29066
v  Velocity[Z]         -0.0017452       0.0019809      9.1905e-08      1.7921e-09
v  ǁVelocityǁ            0.015691          12.143          6.8324          4.2217
v  Pressure                1904.7           69067           48000           58148
v  Void Fraction       1.1063e-13         0.93182       0.0032057      5.5566e-05
v  k                   3.9201e-19          1.6115        0.014564         0.02189
v  omega               1.7229e-11      2.3501e+11      6.9545e+06      1.5629e+05
v  scalar1                      0               0               0               0
v  TurbVisc            8.9431e-25         0.24338         0.01369         0.12689
v  CourantNb           0.00062652          4.6542         0.85489         0.11994
v  FourierNb            0.0057829         0.80936         0.12302        0.073819
v  total_pressure          1904.7           69067           48000           58148
v  Density Old             73.006            1000          996.96          999.95


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01621          4.9537         0.97791         0.19376


 TIME FOR THE TIME STEP               53:        0.15258E+01

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


 INSTANT    0.270000000E-03   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158847073E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18733E+01
   Friction velocity        uet   :  0.38747E-01 0.11439E+01
   Friction velocity        uk    :  0.38747E-01 0.14871E+01
   Dimensionless distance   yplus :  0.96867E-01 0.35931E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1103
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1765E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43773E-01      23   0.39848E-04   0.29622E+01 0.17288E+03 
c  Velocity[X]                                      0.25589E+01 
c  Velocity[Y]                                      0.40328E+00 
c  Velocity[Z]                                      0.19390E-07 
c  Pressure     0.10905E-09    1922   0.18070E-02   0.17075E+00 0.74439E+03 
c  Void Fractio 0.21211E-08      38   0.49517E-08   0.97140E-02 0.94811E+04 
c  k            0.29578E-03      22   0.20572E-05   0.16047E-01 0.24592E+04 
c  omega        0.22182E+10       3   0.16506E-07   0.74572E+21 0.19994E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.8985e-07                            12
a  omega             -6.2828e+07                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9651          12.121          6.7779          4.2037
v  Velocity[Y]             -2.483           3.091        -0.10413        -0.29071
v  Velocity[Z]         -0.0018975         0.00211      9.7689e-08      1.9248e-09
v  ǁVelocityǁ           0.0093253          12.124          6.8285          4.2222
v  Pressure                1877.5           68630           47610           57975
v  Void Fraction       9.1072e-14         0.93107       0.0032899      5.7336e-05
v  k                   4.7024e-19          1.5954        0.014547        0.021888
v  omega               8.6954e-12      1.1751e+11      4.0007e+06        1.13e+05
v  scalar1                      0               0               0               0
v  TurbVisc            5.2609e-24         0.24338        0.013669         0.12684
v  CourantNb           0.00062113          4.6496         0.85445         0.11995
v  FourierNb            0.0057902         0.80702         0.12295        0.073661
v  total_pressure          1877.5           68630           47610           57975
v  Density Old             69.573            1000          996.88          999.95


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016216          4.9392          0.9774         0.19361


 TIME FOR THE TIME STEP               54:        0.15648E+01

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


 INSTANT    0.275000000E-03   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158867471E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18802E+01
   Friction velocity        uet   :  0.56310E-02 0.99955E+00
   Friction velocity        uk    :  0.56310E-02 0.14852E+01
   Dimensionless distance   yplus :  0.14078E-01 0.35885E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1104
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.3144E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43780E-01      23   0.41547E-04   0.29605E+01 0.17281E+03 
c  Velocity[X]                                      0.25369E+01 
c  Velocity[Y]                                      0.42357E+00 
c  Velocity[Z]                                      0.27208E-07 
c  Pressure     0.16575E-08    1643   0.69228E-03   0.10034E+01 0.39382E+03 
c  Void Fractio 0.21632E-08      37   0.59360E-08   0.10039E-01 0.94568E+04 
c  k            0.29578E-03      23   0.11382E-05   0.66467E-02 0.15829E+04 
c  omega        0.55475E+09       3   0.32356E-07   0.18643E+21 0.19976E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.4722e-07                            12
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9987          12.089          6.7737          4.2042
v  Velocity[Y]             -2.498          3.0912        -0.10386        -0.29077
v  Velocity[Z]         -0.0020479       0.0023716      9.8212e-08      1.9366e-09
v  ǁVelocityǁ            0.014206          12.094          6.8247          4.2226
v  Pressure                1906.7           68349           47402           57884
v  Void Fraction       7.4987e-14         0.93396       0.0033749      5.9133e-05
v  k                   5.6151e-19          1.5954        0.014536        0.021887
v  omega               5.4498e-12      5.8752e+10      2.5216e+06           91303
v  scalar1                      0               0               0               0
v  TurbVisc            1.0055e-23         0.24338        0.013649         0.12679
v  CourantNb           0.00061591          4.6559         0.85404         0.11997
v  FourierNb            0.0057976         0.80479         0.12288        0.073502
v  total_pressure          1906.7           68349           47402           57884
v  Density Old              69.11            1000           996.8          999.94


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016222          4.9464         0.97692         0.19347


 TIME FOR THE TIME STEP               55:        0.13924E+01

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


 INSTANT    0.280000000E-03   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158887495E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18828E+01
   Friction velocity        uet   :  0.21881E-01 0.11194E+01
   Friction velocity        uk    :  0.21881E-01 0.14811E+01
   Dimensionless distance   yplus :  0.54703E-01 0.35786E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1105
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1764E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43788E-01      23   0.39925E-04   0.28789E+01 0.17039E+03 
c  Velocity[X]                                      0.24676E+01 
c  Velocity[Y]                                      0.41138E+00 
c  Velocity[Z]                                      0.20516E-07 
c  Pressure     0.15388E-09    1932   0.19513E-02   0.23948E+00 0.53109E+03 
c  Void Fractio 0.22051E-08      37   0.46508E-08   0.96766E-02 0.91138E+04 
c  k            0.29578E-03      22   0.11996E-05   0.73742E-02 0.16674E+04 
c  omega        0.13989E+09       4   0.62892E-07   0.46614E+20 0.19906E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.9606e-07                            12
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0098          12.073          6.7696          4.2047
v  Velocity[Y]            -2.5264          3.1028        -0.10359        -0.29082
v  Velocity[Z]         -0.0021875       0.0026119      1.0163e-07      2.0297e-09
v  ǁVelocityǁ            0.009684          12.078          6.8209          4.2231
v  Pressure                1906.9           68014           47124           57761
v  Void Fraction        6.176e-14         0.93474       0.0034606      6.0955e-05
v  k                   6.6757e-19          1.6002        0.014527        0.021886
v  omega               4.8551e-12      2.9374e+10      1.7837e+06           80442
v  scalar1                      0               0               0               0
v  TurbVisc            1.2007e-23         0.24339        0.013629         0.12674
v  CourantNb           0.00061079          4.6435         0.85363         0.11998
v  FourierNb             0.005805         0.80276         0.12281        0.073346
v  total_pressure          1906.9           68014           47124           57761
v  Density Old             69.865            1000          996.71          999.94


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016227          4.9344         0.97644         0.19333


 TIME FOR THE TIME STEP               56:        0.15419E+01

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


 INSTANT    0.285000000E-03   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158906967E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18723E+01
   Friction velocity        uet   :  0.41521E-01 0.98729E+00
   Friction velocity        uk    :  0.41521E-01 0.14773E+01
   Dimensionless distance   yplus :  0.10380E+00 0.35695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1105
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2175E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43794E-01      23   0.39192E-04   0.27964E+01 0.16791E+03 
c  Velocity[X]                                      0.23953E+01 
c  Velocity[Y]                                      0.40112E+00 
c  Velocity[Z]                                      0.12422E-07 
c  Pressure     0.69509E-09    1842   0.13576E-02   0.80186E+00 0.40925E+03 
c  Void Fractio 0.22472E-08      37   0.52049E-08   0.94913E-02 0.88630E+04 
c  k            0.29578E-03      23   0.11552E-05   0.65514E-02 0.15718E+04 
c  omega        0.35508E+08       5   0.12228E-06   0.11654E+20 0.19627E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.2215e-07                            11
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9903          12.042          6.7655          4.2051
v  Velocity[Y]            -2.5367          3.1032        -0.10333        -0.29087
v  Velocity[Z]         -0.0023065       0.0028358      1.0396e-07      2.0846e-09
v  ǁVelocityǁ            0.015514          12.045          6.8172          4.2236
v  Pressure                1572.4           67771           46907           57668
v  Void Fraction       5.0877e-14         0.93394       0.0035468      6.2802e-05
v  k                   7.9038e-19          1.5914        0.014521        0.021885
v  omega                 6.08e-12      1.4684e+10      1.4112e+06           74925
v  scalar1                      0               0               0               0
v  TurbVisc            1.4275e-23         0.24339        0.013609         0.12669
v  CourantNb           0.00060565          4.6402         0.85321         0.11999
v  FourierNb            0.0058123         0.80091         0.12274        0.073191
v  total_pressure          1572.4           67771           46907           57668
v  Density Old             66.974            1000          996.63          999.94


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016233          4.9314         0.97594         0.19318


 TIME FOR THE TIME STEP               57:        0.15561E+01

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


 INSTANT    0.290000000E-03   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158926046E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18580E+01
   Friction velocity        uet   :  0.56223E-01 0.11122E+01
   Friction velocity        uk    :  0.56223E-01 0.14757E+01
   Dimensionless distance   yplus :  0.14056E+00 0.35655E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1106
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1507E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43801E-01      23   0.37820E-04   0.27521E+01 0.16655E+03 
c  Velocity[X]                                      0.23464E+01 
c  Velocity[Y]                                      0.40575E+00 
c  Velocity[Z]                                      0.11086E-07 
c  Pressure     0.55145E-08    1475   0.20765E-03   0.10167E+01 0.40751E+03 
c  Void Fractio 0.22905E-08      37   0.57444E-08   0.10585E-01 0.91936E+04 
c  k            0.29578E-03      23   0.10086E-05   0.47962E-02 0.13449E+04 
c  omega        0.77133E+07       7   0.28949E-06   0.29142E+19 0.18608E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.9963e-07                            10
a  omega             -9.0091e+05                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9657          12.022          6.7615          4.2056
v  Velocity[Y]            -2.5521          3.0888        -0.10307        -0.29092
v  Velocity[Z]         -0.0023797       0.0029959      1.0513e-07      2.1183e-09
v  ǁVelocityǁ            0.013651          12.028          6.8135           4.224
v  Pressure                1907.9           67517           46695           57573
v  Void Fraction       4.1918e-14         0.93743       0.0036334      6.4673e-05
v  k                   9.3206e-19          1.5816        0.014521        0.021885
v  omega               1.4593e-12      7.3404e+09      1.2271e+06           72175
v  scalar1                      0               0               0               0
v  TurbVisc            1.6901e-23         0.24339        0.013589         0.12664
v  CourantNb           0.00060068          4.6177         0.85279         0.12001
v  FourierNb            0.0058197         0.79906         0.12266         0.07304
v  total_pressure          1907.9           67517           46695           57573
v  Density Old             66.196            1000          996.54          999.94


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016239          4.9095         0.97546         0.19305


 TIME FOR THE TIME STEP               58:        0.13463E+01

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


 INSTANT    0.295000000E-03   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158944708E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18541E+01
   Friction velocity        uet   :  0.64994E-01 0.98103E+00
   Friction velocity        uk    :  0.64993E-01 0.14713E+01
   Dimensionless distance   yplus :  0.16248E+00 0.35549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1107
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1774E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43808E-01      23   0.38814E-04   0.26702E+01 0.16403E+03 
c  Velocity[X]                                      0.22903E+01 
c  Velocity[Y]                                      0.37992E+00 
c  Velocity[Z]                                      0.12100E-07 
c  Pressure     0.51954E-09    1882   0.14227E-02   0.66285E+00 0.47846E+03 
c  Void Fractio 0.23336E-08      37   0.60046E-08   0.98457E-02 0.87136E+04 
c  k            0.29578E-03      23   0.10245E-05   0.57320E-02 0.14705E+04 
c  omega        0.19230E+07       9   0.58685E-06   0.73169E+18 0.15748E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -9.1078e-08                             9
a  omega             -2.7183e+06                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9816          12.002          6.7575           4.206
v  Velocity[Y]            -2.5773          3.0679         -0.1028        -0.29097
v  Velocity[Z]         -0.0024865       0.0031493      1.0659e-07      2.1456e-09
v  ǁVelocityǁ            0.018915          12.012          6.8099          4.2245
v  Pressure                  1909           67197           46443           57465
v  Void Fraction       3.4547e-14         0.93836       0.0037208      6.6568e-05
v  k                    1.095e-18          1.5573        0.014518        0.021884
v  omega               1.6866e-13      3.6631e+09      1.1332e+06           70752
v  scalar1                      0               0               0               0
v  TurbVisc             1.993e-23          0.2434         0.01357         0.12659
v  CourantNb           0.00059587          4.6025         0.85239         0.12002
v  FourierNb            0.0058271         0.80227          0.1226        0.072891
v  total_pressure            1909           67197           46443           57465
v  Density Old             66.998            1000          996.46          999.94


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016244          4.8948         0.97498         0.19291


 TIME FOR THE TIME STEP               59:        0.15607E+01

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


 INSTANT    0.300000000E-03   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158962906E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18564E+01
   Friction velocity        uet   :  0.74982E-01 0.11153E+01
   Friction velocity        uk    :  0.74982E-01 0.14677E+01
   Dimensionless distance   yplus :  0.18746E+00 0.35462E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1108
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1758E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43814E-01      22   0.39612E-04   0.25987E+01 0.16180E+03 
c  Velocity[X]                                      0.22336E+01 
c  Velocity[Y]                                      0.36505E+00 
c  Velocity[Z]                                      0.10412E-07 
c  Pressure     0.58835E-09    1968   0.14934E-02   0.74651E+00 0.41236E+03 
c  Void Fractio 0.23750E-08      37   0.61177E-08   0.87009E-02 0.80525E+04 
c  k            0.29578E-03      23   0.11087E-05   0.63834E-02 0.15519E+04 
c  omega        0.50335E+06      11   0.11833E-05   0.18380E+18 0.10745E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -7.4818e-08                             9
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.015          11.982          6.7535          4.2064
v  Velocity[Y]            -2.5892          3.0683        -0.10254        -0.29102
v  Velocity[Z]         -0.0025511       0.0032735      1.0717e-07      2.1579e-09
v  ǁVelocityǁ            0.015254          12.016          6.8063          4.2249
v  Pressure                1632.1           66956           46228           57370
v  Void Fraction       2.8477e-14         0.93983       0.0038085      6.8486e-05
v  k                   1.2816e-18          1.5612        0.014517        0.021884
v  omega               5.1245e-14      1.8264e+09      1.0876e+06           70031
v  scalar1                      0               0               0               0
v  TurbVisc            2.3414e-23          0.2434        0.013551         0.12654
v  CourantNb           0.00059115          4.5981         0.85199         0.12003
v  FourierNb            0.0058346         0.82918         0.12253        0.072745
v  total_pressure          1632.1           66956           46228           57370
v  Density Old             63.505            1000          996.37          999.94


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01625          4.8908         0.97452         0.19278


 TIME FOR THE TIME STEP               60:        0.16091E+01

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


 INSTANT    0.305000000E-03   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158980687E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18649E+01
   Friction velocity        uet   :  0.75743E-01 0.98421E+00
   Friction velocity        uk    :  0.75738E-01 0.14658E+01
   Dimensionless distance   yplus :  0.18751E+00 0.35415E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1108
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.4056E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43821E-01      23   0.38522E-04   0.25397E+01 0.15994E+03 
c  Velocity[X]                                      0.21867E+01 
c  Velocity[Y]                                      0.35306E+00 
c  Velocity[Z]                                      0.81691E-08 
c  Pressure     0.46308E-08    1707   0.23371E-03   0.10164E+01 0.45414E+03 
c  Void Fractio 0.24184E-08      37   0.47754E-08   0.91884E-02 0.81379E+04 
c  k            0.29579E-03      23   0.10758E-05   0.53778E-02 0.14246E+04 
c  omega        0.16557E+06      13   0.18160E-05   0.45733E+17 0.60442E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -8.098e-08                             9
a  omega             -6.0942e+05                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9878          11.976          6.7496          4.2068
v  Velocity[Y]            -2.6048          3.0812        -0.10228        -0.29106
v  Velocity[Z]         -0.0025896       0.0033665      1.0933e-07      2.2071e-09
v  ǁVelocityǁ              0.0214          12.005          6.8027          4.2253
v  Pressure                1744.7           66641           45991           57267
v  Void Fraction       2.3479e-14         0.94138       0.0038964      7.0427e-05
v  k                   1.4949e-18          1.5739        0.014515        0.021883
v  omega               1.6989e-14      9.0952e+08       1.062e+06           69601
v  scalar1                      0               0               0               0
v  TurbVisc            2.7405e-23          0.2434        0.013532          0.1265
v  CourantNb           0.00058651           4.575         0.85156         0.12004
v  FourierNb            0.0058421         0.84976         0.12246          0.0726
v  total_pressure          1744.7           66641           45991           57267
v  Density Old             62.579            1000          996.28          999.93


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016256           4.868         0.97402         0.19264


 TIME FOR THE TIME STEP               61:        0.16153E+01

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


 INSTANT    0.310000000E-03   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158998010E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18648E+01
   Friction velocity        uet   :  0.84449E-01 0.11181E+01
   Friction velocity        uk    :  0.84449E-01 0.14624E+01
   Dimensionless distance   yplus :  0.21112E+00 0.35335E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1109
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.2318E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43827E-01      22   0.37205E-04   0.25848E+01 0.16133E+03 
c  Velocity[X]                                      0.22362E+01 
c  Velocity[Y]                                      0.34860E+00 
c  Velocity[Z]                                      0.46133E-08 
c  Pressure     0.32883E-08    1691   0.30731E-03   0.10129E+01 0.34841E+03 
c  Void Fractio 0.24616E-08      37   0.47512E-08   0.88923E-02 0.78753E+04 
c  k            0.29579E-03      23   0.10542E-05   0.48069E-02 0.13469E+04 
c  omega        0.93707E+05      14   0.24111E-05   0.12349E+17 0.32473E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.2697e-08                             9
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0333          11.975          6.7456          4.2072
v  Velocity[Y]             -2.634          3.0753        -0.10201        -0.29111
v  Velocity[Z]         -0.0026306       0.0034431      1.0767e-07      2.1804e-09
v  ǁVelocityǁ            0.018516              12          6.7992          4.2257
v  Pressure                1907.9           66381           45806           57189
v  Void Fraction       1.9361e-14         0.94143       0.0039847       7.239e-05
v  k                   1.7377e-18          1.5671        0.014521        0.021883
v  omega               1.1436e-14      4.5427e+08      1.0519e+06           69407
v  scalar1                      0               0               0               0
v  TurbVisc            3.1965e-23         0.24341        0.013514         0.12645
v  CourantNb           0.00058198          4.5826         0.85118         0.12005
v  FourierNb            0.0058497         0.85368         0.12239        0.072458
v  total_pressure          1907.9           66381           45806           57189
v  Density Old             61.111            1000           996.2          999.93


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016261          4.8758         0.97357         0.19251


 TIME FOR THE TIME STEP               62:        0.15795E+01

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


 INSTANT    0.315000000E-03   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159015022E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18643E+01
   Friction velocity        uet   :  0.85483E-01 0.98683E+00
   Friction velocity        uk    :  0.85478E-01 0.14598E+01
   Dimensionless distance   yplus :  0.21159E+00 0.35270E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1110
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1578E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43833E-01      22   0.37023E-04   0.24513E+01 0.15709E+03 
c  Velocity[X]                                      0.21355E+01 
c  Velocity[Y]                                      0.31585E+00 
c  Velocity[Z]                                      0.83968E-08 
c  Pressure     0.14024E-09    1950   0.15794E-02   0.23333E+00 0.47942E+03 
c  Void Fractio 0.25058E-08      38   0.61437E-08   0.86126E-02 0.76265E+04 
c  k            0.29579E-03      23   0.10818E-05   0.61323E-02 0.15214E+04 
c  omega        0.19698E+14       2   0.29890E-13   0.32995E+16 0.16945E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -3.283e-08                             6
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0425          11.968          6.7417          4.2076
v  Velocity[Y]            -2.6455          3.0677        -0.10175        -0.29116
v  Velocity[Z]         -0.0026391       0.0034829       1.065e-07      2.1471e-09
v  ǁVelocityǁ            0.023477          11.994          6.7958          4.2261
v  Pressure                1782.1           66083           45557           57080
v  Void Fraction        1.597e-14         0.94025       0.0040731      7.4375e-05
v  k                   2.0134e-18          1.5601        0.014523        0.021882
v  omega               2.1979e-09      2.2667e+08      1.0457e+06           69281
v  scalar1                      0               0               0               0
v  TurbVisc            3.7158e-23         0.24341        0.013496         0.12641
v  CourantNb           0.00057761          4.5871         0.85078         0.12007
v  FourierNb            0.0058572          0.8392         0.12233        0.072318
v  total_pressure          1782.1           66083           45557           57080
v  Density Old             59.565            1000          996.11          999.93


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016267          4.8806         0.97311         0.19238


 TIME FOR THE TIME STEP               63:        0.16966E+01

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


 INSTANT    0.320000000E-03   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159031542E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18777E+01
   Friction velocity        uet   :  0.91096E-01 0.89981E+00
   Friction velocity        uk    :  0.91096E-01 0.14564E+01
   Dimensionless distance   yplus :  0.22774E+00 0.35189E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1110
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1777E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43839E-01      23   0.37491E-04   0.25505E+01 0.16022E+03 
c  Velocity[X]                                      0.22305E+01 
c  Velocity[Y]                                      0.31997E+00 
c  Velocity[Z]                                      0.54363E-08 
c  Pressure     0.29166E-08    1571   0.31767E-03   0.10216E+01 0.31198E+03 
c  Void Fractio 0.25518E-08      38   0.52723E-08   0.92270E-02 0.77684E+04 
c  k            0.29579E-03      23   0.36936E-06   0.19973E-02 0.86832E+03 
c  omega        0.86049E+05      14   0.61155E-06   0.77470E+15 0.82326E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.9743e-08                             6
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0806          11.958          6.7377           4.208
v  Velocity[Y]            -2.6689          3.0643        -0.10148         -0.2912
v  Velocity[Z]         -0.0026611       0.0035336      1.0723e-07      2.1503e-09
v  ǁVelocityǁ            0.023439          11.978          6.7923          4.2265
v  Pressure                1900.8           65865           45392           57011
v  Void Fraction       1.3175e-14         0.93842       0.0041618       7.638e-05
v  k                   2.3257e-18          1.5642        0.014532        0.021882
v  omega               8.1388e-10      1.1315e+08      1.0417e+06           69172
v  scalar1                      0               0               0               0
v  TurbVisc            4.3054e-23         0.24341        0.013479         0.12636
v  CourantNb            0.0005733          4.5818          0.8504         0.12008
v  FourierNb            0.0058648         0.83234         0.12228        0.072184
v  total_pressure          1900.8           65865           45392           57011
v  Density Old             59.516            1000          996.02          999.93


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016273          4.8753         0.97269         0.19226


 TIME FOR THE TIME STEP               64:        0.13840E+01

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


 INSTANT    0.325000000E-03   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159047786E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18849E+01
   Friction velocity        uet   :  0.97291E-01 0.11043E+01
   Friction velocity        uk    :  0.97287E-01 0.14538E+01
   Dimensionless distance   yplus :  0.24081E+00 0.35125E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1111
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2192E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43845E-01      23   0.38222E-04   0.24185E+01 0.15601E+03 
c  Velocity[X]                                      0.21167E+01 
c  Velocity[Y]                                      0.30182E+00 
c  Velocity[Z]                                      0.34163E-08 
c  Pressure     0.11741E-09    1892   0.16770E-02   0.19605E+00 0.37525E+03 
c  Void Fractio 0.25948E-08      37   0.57471E-08   0.79843E-02 0.71143E+04 
c  k            0.29579E-03      23   0.10826E-05   0.47574E-02 0.13402E+04 
c  omega        0.86011E+05      13   0.24241E-05   0.18852E+16 0.12825E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.8969e-14                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1086          11.949          6.7339          4.2083
v  Velocity[Y]            -2.6731          3.0574        -0.10122        -0.29125
v  Velocity[Z]         -0.0026979       0.0035792      1.0708e-07      2.1384e-09
v  ǁVelocityǁ             0.02321          11.971           6.789          4.2269
v  Pressure                1818.8           65652           45198           56925
v  Void Fraction        1.087e-14         0.93629       0.0042507      7.8407e-05
v  k                   2.6783e-18          1.5582        0.014539        0.021882
v  omega               3.3321e-11      1.7782e+08      1.0433e+06           69158
v  scalar1                      0               0               0               0
v  TurbVisc             4.973e-23         0.24342        0.013462         0.12632
v  CourantNb           0.00056909          4.5505         0.85002         0.12009
v  FourierNb            0.0058724         0.83253         0.12222        0.072049
v  total_pressure          1818.8           65652           45198           56925
v  Density Old             60.686            1000          995.93          999.93


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016279          4.8444         0.97224         0.19214


 TIME FOR THE TIME STEP               65:        0.15278E+01

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


 INSTANT    0.330000000E-03   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159063654E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18864E+01
   Friction velocity        uet   :  0.31998E-01 0.97965E+00
   Friction velocity        uk    :  0.31994E-01 0.14510E+01
   Dimensionless distance   yplus :  0.79094E-01 0.35060E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1112
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1126E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43851E-01      23   0.38500E-04   0.24809E+01 0.15799E+03 
c  Velocity[X]                                      0.21773E+01 
c  Velocity[Y]                                      0.30360E+00 
c  Velocity[Z]                                      0.78919E-08 
c  Pressure     0.22182E-08    1526   0.36848E-03   0.10090E+01 0.29876E+03 
c  Void Fractio 0.26387E-08      37   0.51661E-08   0.79262E-02 0.69801E+04 
c  k            0.29579E-03      23   0.12481E-05   0.74041E-02 0.16721E+04 
c  omega        0.86066E+05      13   0.12357E-05   0.68040E+15 0.77145E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.1554e-14                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1503          11.945            6.73          4.2087
v  Velocity[Y]            -2.6723          3.0596        -0.10095        -0.29129
v  Velocity[Z]         -0.0026968       0.0035875      1.0364e-07        2.05e-09
v  ǁVelocityǁ            0.024538          11.963          6.7856          4.2273
v  Pressure                1890.3           65411           45039           56860
v  Void Fraction       8.9707e-15         0.93401       0.0043395      8.0453e-05
v  k                   3.0754e-18          1.5502        0.014541        0.021882
v  omega               1.5952e-12      9.5961e+07      1.0418e+06           69100
v  scalar1                      0               0               0               0
v  TurbVisc             5.727e-23         0.24342        0.013445         0.12628
v  CourantNb           0.00056486          4.5543         0.84964          0.1201
v  FourierNb              0.00588         0.83423         0.12216        0.071916
v  total_pressure          1890.3           65411           45039           56860
v  Density Old             62.517            1000          995.84          999.92


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016284          4.8486          0.9718         0.19202


 TIME FOR THE TIME STEP               66:        0.13302E+01

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


 INSTANT    0.335000000E-03   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159079266E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18948E+01
   Friction velocity        uet   :  0.96010E-01 0.89226E+00
   Friction velocity        uk    :  0.96010E-01 0.14493E+01
   Dimensionless distance   yplus :  0.23763E+00 0.35017E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1113
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1763E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43857E-01      23   0.38585E-04   0.23686E+01 0.15435E+03 
c  Velocity[X]                                      0.20795E+01 
c  Velocity[Y]                                      0.28910E+00 
c  Velocity[Z]                                      0.34603E-07 
c  Pressure     0.23340E-09    1804   0.14321E-02   0.39318E+00 0.40219E+03 
c  Void Fractio 0.26858E-08      37   0.50495E-08   0.78648E-02 0.68479E+04 
c  k            0.29579E-03      22   0.57357E-06   0.44694E-02 0.12992E+04 
c  omega        0.86016E+05      12   0.12020E-05   0.84003E+15 0.85697E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.4424e-14                             5
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1777          11.931          6.7261          4.2091
v  Velocity[Y]            -2.6825          3.0573        -0.10068        -0.29134
v  Velocity[Z]         -0.0026687       0.0034724      9.7981e-08      1.9058e-09
v  ǁVelocityǁ           0.0035573          11.952          6.7823          4.2277
v  Pressure                1850.7           65149           44831           56769
v  Void Fraction       7.4045e-15         0.93948       0.0044286       8.252e-05
v  k                   3.5215e-18          1.5649        0.014547        0.021882
v  omega               3.7019e-14      9.7702e+07      1.0419e+06           69071
v  scalar1                      0               0               0               0
v  TurbVisc            6.5762e-23         0.24342        0.013428         0.12624
v  CourantNb           0.00056081          4.5589         0.84925         0.12011
v  FourierNb            0.0058876         0.83378         0.12211        0.071786
v  total_pressure          1850.7           65149           44831           56769
v  Density Old             64.644            1000          995.75          999.92


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01629          4.8535         0.97136          0.1919


 TIME FOR THE TIME STEP               67:        0.14622E+01

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


 INSTANT    0.340000000E-03   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159094474E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18787E+01
   Friction velocity        uet   :  0.26999E-01 0.10994E+01
   Friction velocity        uk    :  0.26999E-01 0.14467E+01
   Dimensionless distance   yplus :  0.66824E-01 0.34955E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1115
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1158E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43862E-01      23   0.38593E-04   0.24347E+01 0.15648E+03 
c  Velocity[X]                                      0.21435E+01 
c  Velocity[Y]                                      0.29119E+00 
c  Velocity[Z]                                      0.18500E-07 
c  Pressure     0.17890E-08    1518   0.49747E-03   0.10063E+01 0.16662E+03 
c  Void Fractio 0.27300E-08      37   0.46850E-08   0.77427E-02 0.66933E+04 
c  k            0.29579E-03      22   0.11694E-05   0.87666E-02 0.18197E+04 
c  omega        0.86020E+05      12   0.24412E-05   0.19287E+16 0.12967E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.7601e-14                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2229          11.919          6.7222          4.2094
v  Velocity[Y]            -2.6875          3.0551        -0.10042        -0.29138
v  Velocity[Z]         -0.0026363       0.0032937      9.1757e-08      1.7755e-09
v  ǁVelocityǁ            0.018071          11.941           6.779           4.228
v  Pressure                  1898           65067           44743           56732
v  Void Fraction       6.1122e-15         0.94059       0.0045177      8.4606e-05
v  k                   4.0216e-18          1.5406        0.014547        0.021881
v  omega               3.4481e-16      1.6929e+08      1.0445e+06           69078
v  scalar1                      0               0               0               0
v  TurbVisc            7.5302e-23         0.24343        0.013412          0.1262
v  CourantNb           0.00055674          4.5475         0.84888         0.12012
v  FourierNb            0.0058953         0.83191         0.12205        0.071657
v  total_pressure            1898           65067           44743           56732
v  Density Old             66.919            1000          995.66          999.92


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016296          4.8424         0.97094         0.19178


 TIME FOR THE TIME STEP               68:        0.13238E+01

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


 INSTANT    0.345000000E-03   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159109552E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18740E+01
   Friction velocity        uet   :  0.87939E-01 0.97576E+00
   Friction velocity        uk    :  0.87939E-01 0.14450E+01
   Dimensionless distance   yplus :  0.21765E+00 0.34913E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1115
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2010E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43868E-01      22   0.36935E-04   0.23624E+01 0.15412E+03 
c  Velocity[X]                                      0.20793E+01 
c  Velocity[Y]                                      0.28310E+00 
c  Velocity[Z]                                      0.13553E-07 
c  Pressure     0.48935E-09    1896   0.11349E-02   0.66952E+00 0.29530E+03 
c  Void Fractio 0.27771E-08      37   0.59927E-08   0.79506E-02 0.66826E+04 
c  k            0.29580E-03      22   0.12118E-05   0.70620E-02 0.16335E+04 
c  omega        0.86058E+05      12   0.10803E-05   0.41654E+15 0.60360E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -3.108e-14                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2545          11.912          6.7184          4.2098
v  Velocity[Y]            -2.7027          3.0552        -0.10016        -0.29142
v  Velocity[Z]         -0.0024571       0.0032402      9.2684e-08      1.7884e-09
v  ǁVelocityǁ            0.006601          11.928          6.7758          4.2284
v  Pressure                1898.1           64868           44589           56666
v  Void Fraction       5.0461e-15         0.94076        0.004607      8.6711e-05
v  k                   4.5807e-18          1.5374        0.014545        0.021881
v  omega                3.069e-18      9.2042e+07      1.0419e+06           68993
v  scalar1                      0               0               0               0
v  TurbVisc            8.5994e-23         0.24343        0.013396         0.12615
v  CourantNb           0.00055273            4.54          0.8485         0.12013
v  FourierNb            0.0059029         0.84981           0.122         0.07153
v  total_pressure          1898.1           64868           44589           56666
v  Density Old             61.461            1000          995.58          999.92


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016301           4.835          0.9705         0.19166


 TIME FOR THE TIME STEP               69:        0.15165E+01

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


 INSTANT    0.350000000E-03   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159124345E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18742E+01
   Friction velocity        uet   :  0.47097E-01 0.93489E+00
   Friction velocity        uk    :  0.47097E-01 0.14428E+01
   Dimensionless distance   yplus :  0.11655E+00 0.34860E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1116
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1702E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43873E-01      22   0.37532E-04   0.23731E+01 0.15445E+03 
c  Velocity[X]                                      0.20894E+01 
c  Velocity[Y]                                      0.28373E+00 
c  Velocity[Z]                                      0.17897E-07 
c  Pressure     0.62142E-09    1572   0.10213E-02   0.79526E+00 0.15850E+03 
c  Void Fractio 0.28244E-08      37   0.57474E-08   0.80898E-02 0.66418E+04 
c  k            0.29580E-03      22   0.41368E-06   0.17521E-02 0.81365E+03 
c  omega        0.86024E+05      13   0.70899E-06   0.30509E+15 0.51662E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.4782e-14                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.285          11.912          6.7145          4.2101
v  Velocity[Y]            -2.7144          3.0608         -0.0999        -0.29147
v  Velocity[Z]         -0.0023095       0.0031339      8.4659e-08      1.6365e-09
v  ǁVelocityǁ           0.0091335          11.922          6.7726          4.2287
v  Pressure                  1898           64734           44505           56631
v  Void Fraction       4.1663e-15         0.94048       0.0046964      8.8836e-05
v  k                   5.2044e-18          1.5345        0.014557        0.021881
v  omega               2.3817e-20      5.9153e+07      1.0418e+06           68962
v  scalar1                      0               0               0               0
v  TurbVisc             9.795e-23         0.24343         0.01338         0.12611
v  CourantNb           0.00054886          4.5128         0.84812         0.12014
v  FourierNb            0.0059106         0.82465         0.12195        0.071405
v  total_pressure            1898           64734           44505           56631
v  Density Old             60.353            1000          995.49          999.92


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016307          4.8079         0.97008         0.19155


 TIME FOR THE TIME STEP               70:        0.13638E+01

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


 INSTANT    0.355000000E-03   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159139025E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18723E+01
   Friction velocity        uet   :  0.55456E-01 0.11022E+01
   Friction velocity        uk    :  0.55456E-01 0.14410E+01
   Dimensionless distance   yplus :  0.13723E+00 0.34817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1118
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.7006E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43879E-01      23   0.36738E-04   0.23511E+01 0.15372E+03 
c  Velocity[X]                                      0.20556E+01 
c  Velocity[Y]                                      0.29556E+00 
c  Velocity[Z]                                      0.14958E-07 
c  Pressure     0.13658E-09    1464   0.14542E-02   0.22906E+00 0.57029E+02 
c  Void Fractio 0.28716E-08      37   0.57906E-08   0.73617E-02 0.62441E+04 
c  k            0.29580E-03      22   0.10773E-05   0.56535E-02 0.14616E+04 
c  omega        0.86885E+05      12   0.24738E-05   0.20474E+16 0.13355E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.8794e-14                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3277          11.916          6.7107          4.2105
v  Velocity[Y]            -2.7348          3.0498       -0.099654        -0.29151
v  Velocity[Z]         -0.0024061       0.0032008      8.9175e-08      1.7184e-09
v  ǁVelocityǁ            0.011703          11.927          6.7693          4.2291
v  Pressure                1899.3           64729           44493           56626
v  Void Fraction       3.4398e-15          0.9377       0.0047855       9.098e-05
v  k                   5.8987e-18          1.5323        0.014564        0.021881
v  omega               1.7366e-22      1.7178e+08      1.0456e+06           68996
v  scalar1                      0               0               0               0
v  TurbVisc            1.1129e-22         0.24344        0.013364         0.12608
v  CourantNb           0.00054502          4.5181         0.84775         0.12015
v  FourierNb            0.0059183         0.81737         0.12191        0.071282
v  total_pressure          1899.3           64729           44493           56626
v  Density Old             60.181            1000           995.4          999.91


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016313          4.8135         0.96966         0.19144


 TIME FOR THE TIME STEP               71:        0.12947E+01

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


 INSTANT    0.360000000E-03   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159153719E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18698E+01
   Friction velocity        uet   :  0.49039E-01 0.97884E+00
   Friction velocity        uk    :  0.49038E-01 0.14394E+01
   Dimensionless distance   yplus :  0.12137E+00 0.34778E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1118
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.3239E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43884E-01      23   0.36162E-04   0.23335E+01 0.15313E+03 
c  Velocity[X]                                      0.20402E+01 
c  Velocity[Y]                                      0.29339E+00 
c  Velocity[Z]                                      0.82025E-08 
c  Pressure     0.23942E-09    1770   0.13449E-02   0.38614E+00 0.26723E+03 
c  Void Fractio 0.29201E-08      37   0.66161E-08   0.71732E-02 0.60754E+04 
c  k            0.29580E-03      22   0.12124E-05   0.63021E-02 0.15433E+04 
c  omega        0.86064E+05      13   0.11243E-05   0.44633E+15 0.62461E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -4.3073e-14                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3757          11.909           6.707          4.2108
v  Velocity[Y]            -2.7403          3.0418       -0.099401        -0.29155
v  Velocity[Z]         -0.0022693       0.0030806      8.6228e-08      1.6513e-09
v  ǁVelocityǁ            0.013261          11.917          6.7661          4.2295
v  Pressure                1820.8           64533           44355           56566
v  Void Fraction       2.8404e-15         0.93578       0.0048745      9.3142e-05
v  k                   6.6695e-18          1.5344        0.014569        0.021881
v  omega               1.2917e-24      9.3189e+07      1.0431e+06           68919
v  scalar1                      0               0               0               0
v  TurbVisc            1.2613e-22         0.24344        0.013349         0.12604
v  CourantNb            0.0005413          4.5071         0.84739         0.12017
v  FourierNb            0.0059261         0.80522         0.12186        0.071159
v  total_pressure          1820.8           64533           44355           56566
v  Density Old             60.456            1000          995.31          999.91


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016319          4.8027         0.96924         0.19132


 TIME FOR THE TIME STEP               72:        0.14896E+01

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


 INSTANT    0.365000000E-03   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159168192E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18668E+01
   Friction velocity        uet   :  0.52280E-01 0.89391E+00
   Friction velocity        uk    :  0.52279E-01 0.14378E+01
   Dimensionless distance   yplus :  0.12700E+00 0.34739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1118
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.3945E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43890E-01      22   0.38568E-04   0.24216E+01 0.15598E+03 
c  Velocity[X]                                      0.21208E+01 
c  Velocity[Y]                                      0.30082E+00 
c  Velocity[Z]                                      0.13339E-07 
c  Pressure     0.21239E-08    1320   0.36648E-03   0.10099E+01 0.11694E+03 
c  Void Fractio 0.29684E-08      37   0.61858E-08   0.73374E-02 0.60575E+04 
c  k            0.29580E-03      22   0.17065E-06   0.50372E-03 0.43630E+03 
c  omega        0.86017E+05      13   0.47718E-06   0.78502E+14 0.26205E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -4.7673e-14                             4
a  omega              1.1157e-26                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4076          11.912          6.7032          4.2111
v  Velocity[Y]            -2.7651          3.0346       -0.099154         -0.2916
v  Velocity[Z]         -0.0020734       0.0028512      8.2835e-08      1.5768e-09
v  ǁVelocityǁ           0.0071168          11.912          6.7629          4.2298
v  Pressure                1904.1           64417           44291           56544
v  Void Fraction       2.3457e-15         0.93644       0.0049633      9.5324e-05
v  k                   7.5238e-18           1.533        0.014584        0.021882
v  omega                    1e-24      5.9581e+07      1.0421e+06           68870
v  scalar1                      0               0               0               0
v  TurbVisc            1.4261e-22         0.24344        0.013333           0.126
v  CourantNb           0.00053759          4.5144         0.84703         0.12018
v  FourierNb            0.0059335         0.82313         0.12181        0.071038
v  total_pressure          1904.1           64417           44291           56544
v  Density Old             63.238            1000          995.22          999.91


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016324          4.8096         0.96884         0.19121


 TIME FOR THE TIME STEP               73:        0.12621E+01

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


 INSTANT    0.370000000E-03   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159182613E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18453E+01
   Friction velocity        uet   :  0.29807E-01 0.11071E+01
   Friction velocity        uk    :  0.29807E-01 0.14363E+01
   Dimensionless distance   yplus :  0.72409E-01 0.34702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1119
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.7000E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43895E-01      22   0.40911E-04   0.24585E+01 0.15715E+03 
c  Velocity[X]                                      0.21522E+01 
c  Velocity[Y]                                      0.30630E+00 
c  Velocity[Z]                                      0.93063E-08 
c  Pressure     0.22845E-09    1670   0.15034E-02   0.37209E+00 0.63967E+02 
c  Void Fractio 0.30182E-08      37   0.56405E-08   0.73696E-02 0.59859E+04 
c  k            0.29580E-03      23   0.10171E-05   0.41398E-02 0.12508E+04 
c  omega        0.23508E+07       7   0.84439E-07   0.15655E+16 0.11682E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -5.257e-14                             4
a  omega              1.4658e-26                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4376          11.913          6.6994          4.2115
v  Velocity[Y]            -2.7748          3.0445       -0.098908        -0.29164
v  Velocity[Z]         -0.0019558       0.0026532      8.0527e-08      1.5267e-09
v  ǁVelocityǁ           0.0093749          11.913          6.7598          4.2302
v  Pressure                  1910           64410           44271           56535
v  Void Fraction        1.937e-15         0.93757       0.0050519      9.7524e-05
v  k                   8.4692e-18          1.5177        0.014594        0.021882
v  omega                    1e-24      1.7055e+08       1.045e+06           68886
v  scalar1                      0               0               0               0
v  TurbVisc            1.6088e-22         0.24345        0.013318         0.12596
v  CourantNb           0.00053397          4.5151         0.84667         0.12019
v  FourierNb            0.0059409         0.79757         0.12177        0.070919
v  total_pressure            1910           64410           44271           56535
v  Density Old             65.158            1000          995.13          999.91


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01633          4.8099         0.96844         0.19111


 TIME FOR THE TIME STEP               74:        0.14550E+01

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


 INSTANT    0.375000000E-03   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159197019E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18395E+01
   Friction velocity        uet   :  0.49216E-01 0.98330E+00
   Friction velocity        uk    :  0.49215E-01 0.14375E+01
   Dimensionless distance   yplus :  0.11956E+00 0.34733E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1119
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1232E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43901E-01      23   0.41031E-04   0.24803E+01 0.15783E+03 
c  Velocity[X]                                      0.21752E+01 
c  Velocity[Y]                                      0.30518E+00 
c  Velocity[Z]                                      0.69298E-08 
c  Pressure     0.28865E-09    1586   0.12498E-02   0.46199E+00 0.53695E+02 
c  Void Fractio 0.30681E-08      37   0.65436E-08   0.76016E-02 0.59952E+04 
c  k            0.29581E-03      23   0.12067E-05   0.62149E-02 0.15327E+04 
c  omega        0.43609E+17       2   0.71501E-17   0.35165E+15 0.55439E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -5.7796e-14                             4
a  omega              3.0448e-26                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4955          11.916          6.6957          4.2118
v  Velocity[Y]            -2.7938          3.0566       -0.098668        -0.29168
v  Velocity[Z]         -0.0018628       0.0024401      7.5819e-08      1.4251e-09
v  ǁVelocityǁ           0.0099513          11.916          6.7566          4.2305
v  Pressure                1914.4           64354           44244           56528
v  Void Fraction       1.5997e-15         0.93833       0.0051401      9.9743e-05
v  k                   9.5131e-18          1.5024        0.014598        0.021882
v  omega                    1e-24      9.2632e+07      1.0433e+06           68831
v  scalar1                      0               0               0               0
v  TurbVisc             1.811e-22         0.24345        0.013304         0.12592
v  CourantNb           0.00053043          4.5038         0.84631          0.1202
v  FourierNb            0.0059484         0.80752         0.12173        0.070802
v  total_pressure          1914.4           64354           44244           56528
v  Density Old             64.495            1000          995.04           999.9


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016335          4.7981         0.96804           0.191


 TIME FOR THE TIME STEP               75:        0.13991E+01

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


 INSTANT    0.380000000E-03   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159211447E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18388E+01
   Friction velocity        uet   :  0.64091E-01 0.89820E+00
   Friction velocity        uk    :  0.64091E-01 0.14362E+01
   Dimensionless distance   yplus :  0.15569E+00 0.34700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1119
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1259E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43906E-01      23   0.41854E-04   0.24753E+01 0.15765E+03 
c  Velocity[X]                                      0.21492E+01 
c  Velocity[Y]                                      0.32602E+00 
c  Velocity[Z]                                      0.73553E-08 
c  Pressure     0.28253E-09    1608   0.13200E-02   0.46150E+00 0.10288E+03 
c  Void Fractio 0.31197E-08      38   0.57853E-08   0.78129E-02 0.59943E+04 
c  k            0.29581E-03      23   0.19126E-06   0.62544E-03 0.48622E+03 
c  omega        0.19666E+12       2   0.10319E-11   0.66130E+14 0.24049E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -6.3338e-14                             4
a  omega              1.4352e-26                             3
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.533          11.918           6.692          4.2121
v  Velocity[Y]            -2.7965           3.061       -0.098417        -0.29173
v  Velocity[Z]         -0.0017701       0.0022751      7.2538e-08      1.3646e-09
v  ǁVelocityǁ            0.017078          11.919          6.7535          4.2309
v  Pressure                1914.7           64266           44189           56509
v  Void Fraction       1.3211e-15         0.94158        0.005228      0.00010198
v  k                   1.0664e-17          1.5041        0.014613        0.021882
v  omega                    1e-24      5.9389e+07      1.0426e+06           68792
v  scalar1                      0               0               0               0
v  TurbVisc            2.0342e-22         0.24345         0.01329         0.12589
v  CourantNb           0.00052697          4.4939         0.84597         0.12021
v  FourierNb             0.005956         0.82765         0.12171        0.070689
v  total_pressure          1914.7           64266           44189           56509
v  Density Old             63.373            1000          994.95           999.9


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016341          4.7879         0.96767          0.1909


 TIME FOR THE TIME STEP               76:        0.13941E+01

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


 INSTANT    0.385000000E-03   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159225834E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18386E+01
   Friction velocity        uet   :  0.84834E-01 0.11137E+01
   Friction velocity        uk    :  0.84833E-01 0.14350E+01
   Dimensionless distance   yplus :  0.20608E+00 0.34673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1120
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.2580E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43911E-01      23   0.42578E-04   0.25625E+01 0.16039E+03 
c  Velocity[X]                                      0.22224E+01 
c  Velocity[Y]                                      0.34009E+00 
c  Velocity[Z]                                      0.79583E-08 
c  Pressure     0.16379E-09    1562   0.14371E-02   0.27797E+00 0.11486E+03 
c  Void Fractio 0.31725E-08      38   0.54324E-08   0.81574E-02 0.60418E+04 
c  k            0.29581E-03      23   0.10244E-05   0.42722E-02 0.12708E+04 
c  omega        0.86013E+05      12   0.22893E-05   0.15468E+16 0.11611E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -6.921e-14                             4
a  omega              1.2328e-26                             3
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5608           11.92          6.6884          4.2125
v  Velocity[Y]            -2.8134          3.0458       -0.098177        -0.29177
v  Velocity[Z]         -0.0016397       0.0021104      7.0217e-08      1.3233e-09
v  ǁVelocityǁ            0.019893          11.922          6.7504          4.2312
v  Pressure                  1904           64158           44128           56485
v  Void Fraction       1.0911e-15         0.94397       0.0053154      0.00010424
v  k                    1.193e-17          1.5067        0.014623        0.021883
v  omega                    1e-24      1.6975e+08      1.0455e+06           68812
v  scalar1                      0               0               0               0
v  TurbVisc            2.2802e-22         0.24346        0.013277         0.12585
v  CourantNb           0.00052354          4.5079         0.84563         0.12022
v  FourierNb            0.0059636         0.79139         0.12168        0.070577
v  total_pressure            1904           64158           44128           56485
v  Density Old             62.611            1000          994.87           999.9


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016346          4.8019         0.96731          0.1908


 TIME FOR THE TIME STEP               77:        0.13879E+01

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


 INSTANT    0.390000000E-03   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159240150E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18382E+01
   Friction velocity        uet   :  0.92584E-01 0.98919E+00
   Friction velocity        uk    :  0.92583E-01 0.14334E+01
   Dimensionless distance   yplus :  0.22491E+00 0.34633E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1120
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.3320E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43917E-01      23   0.41960E-04   0.26044E+01 0.16168E+03 
c  Velocity[X]                                      0.22609E+01 
c  Velocity[Y]                                      0.34353E+00 
c  Velocity[Z]                                      0.57886E-08 
c  Pressure     0.10212E-08    1530   0.76530E-03   0.94047E+00 0.39784E+02 
c  Void Fractio 0.32252E-08      37   0.53056E-08   0.86843E-02 0.61499E+04 
c  k            0.29581E-03      24   0.11851E-05   0.59242E-02 0.14966E+04 
c  omega        0.21454E+06      10   0.42528E-06   0.34745E+15 0.55099E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -7.5402e-14                             4
a  omega              1.7338e-26                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6182          11.918          6.6847          4.2128
v  Velocity[Y]            -2.8297          3.0464       -0.097942        -0.29181
v  Velocity[Z]          -0.001543       0.0019649      6.8196e-08       1.286e-09
v  ǁVelocityǁ            0.017491          11.921          6.7474          4.2315
v  Pressure                1914.6           64144           44128           56490
v  Void Fraction        9.012e-16         0.94487       0.0054023      0.00010651
v  k                    1.332e-17          1.5145         0.01463        0.021883
v  omega                    1e-24      9.2265e+07      1.0438e+06           68758
v  scalar1                      0               0               0               0
v  TurbVisc            2.5509e-22         0.24346        0.013263         0.12581
v  CourantNb           0.00052014           4.518         0.84529         0.12023
v  FourierNb            0.0059712         0.80822         0.12164        0.070463
v  total_pressure          1914.6           64144           44128           56490
v  Density Old             59.358            1000          994.78           999.9


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016352          4.8111         0.96693         0.19069


 TIME FOR THE TIME STEP               78:        0.13767E+01

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


 INSTANT    0.395000000E-03   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159254544E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18376E+01
   Friction velocity        uet   :  0.73683E-01 0.90391E+00
   Friction velocity        uk    :  0.73681E-01 0.14339E+01
   Dimensionless distance   yplus :  0.18234E+00 0.34646E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1120
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.4611E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43922E-01      24   0.41798E-04   0.25426E+01 0.15973E+03 
c  Velocity[X]                                      0.21900E+01 
c  Velocity[Y]                                      0.35256E+00 
c  Velocity[Z]                                      0.48048E-08 
c  Pressure     0.22480E-09    1662   0.13958E-02   0.37002E+00 0.62612E+02 
c  Void Fractio 0.32798E-08      38   0.50380E-08   0.91962E-02 0.62444E+04 
c  k            0.29581E-03      24   0.16467E-06   0.46980E-03 0.42143E+03 
c  omega        0.11306E+06      11   0.34482E-06   0.65089E+14 0.23855E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -8.1919e-14                             4
a  omega              1.7277e-26                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6512          11.919          6.6812          4.2131
v  Velocity[Y]             -2.845          3.0537       -0.097701        -0.29185
v  Velocity[Z]         -0.0014933       0.0018434      6.3571e-08      1.1774e-09
v  ǁVelocityǁ            0.030646          11.919          6.7444          4.2319
v  Pressure                1914.7           64092           44097           56479
v  Void Fraction       7.4434e-16         0.94772       0.0054888      0.00010881
v  k                   1.4846e-17          1.4912        0.014649        0.021884
v  omega                    1e-24      5.9258e+07       1.043e+06           68719
v  scalar1                      0               0               0               0
v  TurbVisc            2.8483e-22         0.24346        0.013249         0.12578
v  CourantNb           0.00051684          4.5071         0.84498         0.12024
v  FourierNb            0.0059789         0.82752          0.1216         0.07035
v  total_pressure          1914.7           64092           44097           56479
v  Density Old             56.971            1000          994.69           999.9


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016357          4.7994         0.96658         0.19059


 TIME FOR THE TIME STEP               79:        0.14304E+01

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


 INSTANT    0.400000000E-03   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159268928E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18372E+01
   Friction velocity        uet   :  0.11483E+00 0.11204E+01
   Friction velocity        uk    :  0.11483E+00 0.14338E+01
   Dimensionless distance   yplus :  0.27895E+00 0.34643E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1121
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1197E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43928E-01      23   0.42557E-04   0.25815E+01 0.16094E+03 
c  Velocity[X]                                      0.22084E+01 
c  Velocity[Y]                                      0.37304E+00 
c  Velocity[Z]                                      0.28084E-08 
c  Pressure     0.18686E-09    1526   0.14916E-02   0.31055E+00 0.17444E+03 
c  Void Fractio 0.33359E-08      37   0.67881E-08   0.97508E-02 0.63451E+04 
c  k            0.29581E-03      24   0.10342E-05   0.42445E-02 0.12667E+04 
c  omega        0.13973E+09       4   0.13878E-08   0.15396E+16 0.11582E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -8.8748e-14                             4
a  omega              1.7407e-26                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7232          11.919          6.6776          4.2135
v  Velocity[Y]            -2.8691          3.0439       -0.097455         -0.2919
v  Velocity[Z]         -0.0014662       0.0017663      6.2827e-08       1.161e-09
v  ǁVelocityǁ            0.012091          11.919          6.7414          4.2322
v  Pressure                1828.7           63958           44004           56442
v  Void Fraction       6.1485e-16         0.94896        0.005575      0.00011112
v  k                   1.6515e-17          1.4813        0.014662        0.021884
v  omega                    1e-24      1.6933e+08      1.0458e+06           68741
v  scalar1                      0               0               0               0
v  TurbVisc            3.1745e-22         0.24347        0.013235         0.12574
v  CourantNb           0.00051361          4.4768         0.84467         0.12025
v  FourierNb            0.0059867         0.82343         0.12158         0.07024
v  total_pressure          1828.7           63958           44004           56442
v  Density Old             56.074            1000           994.6          999.89


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016363          4.7688         0.96624         0.19049


 TIME FOR THE TIME STEP               80:        0.13809E+01

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


 INSTANT    0.405000000E-03   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159283179E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18373E+01
   Friction velocity        uet   :  0.63433E-01 0.99570E+00
   Friction velocity        uk    :  0.63431E-01 0.14322E+01
   Dimensionless distance   yplus :  0.15696E+00 0.34605E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1121
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.2039E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43933E-01      22   0.43552E-04   0.26684E+01 0.16361E+03 
c  Velocity[X]                                      0.22808E+01 
c  Velocity[Y]                                      0.38755E+00 
c  Velocity[Z]                                      0.21423E-08 
c  Pressure     0.21813E-08    1284   0.43150E-03   0.10156E+01 0.59560E+02 
c  Void Fractio 0.33917E-08      37   0.63666E-08   0.10540E-01 0.65108E+04 
c  k            0.29582E-03      24   0.12302E-05   0.63522E-02 0.15498E+04 
c  omega        0.86060E+05      12   0.10555E-05   0.34506E+15 0.54901E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -9.5882e-14                             4
a  omega              1.8016e-26                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7859          11.917          6.6741          4.2138
v  Velocity[Y]            -2.8842          3.0397        -0.09722        -0.29194
v  Velocity[Z]         -0.0014361       0.0016939      6.0342e-08      1.1099e-09
v  ǁVelocityǁ            0.042153          11.917          6.7385          4.2326
v  Pressure                1914.5           63895           43976           56436
v  Void Fraction       5.0789e-16         0.94923       0.0056608      0.00011345
v  k                   1.8341e-17          1.4914        0.014672        0.021885
v  omega                    1e-24      9.2071e+07      1.0443e+06           68692
v  scalar1                      0               0               0               0
v  TurbVisc            3.5315e-22         0.24347        0.013222          0.1257
v  CourantNb           0.00051036          4.4849         0.84436         0.12026
v  FourierNb            0.0059945         0.79789         0.12155        0.070132
v  total_pressure          1914.5           63895           43976           56436
v  Density Old             53.228            1000          994.52          999.89


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016369          4.7763         0.96592          0.1904


 TIME FOR THE TIME STEP               81:        0.12460E+01

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


 INSTANT    0.410000000E-03   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159297454E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18371E+01
   Friction velocity        uet   :  0.13134E+00 0.91003E+00
   Friction velocity        uk    :  0.13134E+00 0.14314E+01
   Dimensionless distance   yplus :  0.32577E+00 0.34586E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1121
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1346E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43938E-01      23   0.42507E-04   0.26870E+01 0.16416E+03 
c  Velocity[X]                                      0.22745E+01 
c  Velocity[Y]                                      0.41245E+00 
c  Velocity[Z]                                      0.22725E-08 
c  Pressure     0.13557E-09    1805   0.16663E-02   0.22910E+00 0.18877E+03 
c  Void Fractio 0.34491E-08      36   0.62409E-08   0.11209E-01 0.66279E+04 
c  k            0.29582E-03      25   0.17414E-06   0.58357E-03 0.46973E+03 
c  omega        0.11850E+18       2   0.15605E-17   0.63619E+14 0.23581E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -1.033e-13                             4
a  omega              1.8612e-26                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8205          11.913          6.6706          4.2141
v  Velocity[Y]            -2.9088          3.0487       -0.096972        -0.29198
v  Velocity[Z]         -0.0014129       0.0016342      5.9103e-08      1.0948e-09
v  ǁVelocityǁ            0.033069          11.913          6.7355          4.2329
v  Pressure                1914.5           63739           43876           56395
v  Void Fraction       4.1959e-16         0.95027       0.0057464       0.0001158
v  k                   2.0334e-17          1.4961        0.014692        0.021885
v  omega                    1e-24      5.9192e+07      1.0436e+06           68659
v  scalar1                      0               0               0               0
v  TurbVisc            3.9219e-22         0.24347        0.013209         0.12567
v  CourantNb           0.00050716          4.4916         0.84406         0.12028
v  FourierNb            0.0060023         0.78452         0.12153        0.070025
v  total_pressure          1914.5           63739           43876           56395
v  Density Old             51.993            1000          994.43          999.89


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016374          4.7817         0.96559          0.1903


 TIME FOR THE TIME STEP               82:        0.15069E+01

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


 INSTANT    0.415000000E-03   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159311573E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18369E+01
   Friction velocity        uet   :  0.11634E+00 0.89598E+00
   Friction velocity        uk    :  0.11634E+00 0.14314E+01
   Dimensionless distance   yplus :  0.28787E+00 0.34585E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1121
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.5046E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43943E-01      22   0.44029E-04   0.27681E+01 0.16660E+03 
c  Velocity[X]                                      0.23349E+01 
c  Velocity[Y]                                      0.43320E+00 
c  Velocity[Z]                                      0.19614E-08 
c  Pressure     0.71473E-09    1554   0.11064E-02   0.83097E+00 0.14830E+03 
c  Void Fractio 0.35061E-08      36   0.52697E-08   0.12046E-01 0.67836E+04 
c  k            0.29582E-03      24   0.29685E-06   0.61862E-03 0.48361E+03 
c  omega        0.34576E+14       2   0.37705E-14   0.68412E+13 0.77331E+03 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                   -1.11e-13                             4
a  omega              3.8462e-26                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8379          11.903          6.6671          4.2144
v  Velocity[Y]            -2.9156           3.056       -0.096723        -0.29202
v  Velocity[Z]          -0.001398       0.0015905      5.9548e-08      1.1241e-09
v  ǁVelocityǁ             0.02106          11.903          6.7327          4.2333
v  Pressure                1914.7           63611           43798           56364
v  Void Fraction       3.4667e-16         0.95086       0.0058319      0.00011817
v  k                   2.2506e-17          1.4857        0.014714        0.021886
v  omega                    1e-24      5.2293e+07      1.0434e+06           68633
v  scalar1                      0               0               0               0
v  TurbVisc            4.3481e-22         0.24348        0.013197         0.12564
v  CourantNb           0.00050417          4.4855         0.84377         0.12029
v  FourierNb            0.0060102         0.80131         0.12151        0.069922
v  total_pressure          1914.7           63611           43798           56364
v  Density Old             51.722            1000          994.34          999.89


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01638          4.7743         0.96528         0.19021


 TIME FOR THE TIME STEP               83:        0.13801E+01

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


 INSTANT    0.420000000E-03   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159325589E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18363E+01
   Friction velocity        uet   :  0.75412E-01 0.11171E+01
   Friction velocity        uk    :  0.75412E-01 0.14306E+01
   Dimensionless distance   yplus :  0.18672E+00 0.34565E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1122
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1817E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43949E-01      23   0.44667E-04   0.27729E+01 0.16673E+03 
c  Velocity[X]                                      0.23131E+01 
c  Velocity[Y]                                      0.45975E+00 
c  Velocity[Z]                                      0.25211E-08 
c  Pressure     0.26430E-09    1682   0.17935E-02   0.42769E+00 0.11411E+03 
c  Void Fractio 0.35629E-08      37   0.48473E-08   0.12738E-01 0.68886E+04 
c  k            0.29582E-03      25   0.11978E-05   0.54726E-02 0.14384E+04 
c  omega        0.86014E+05      14   0.25704E-05   0.19699E+16 0.13092E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.1894e-13                             4
a  omega              3.2164e-26                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8848          11.892          6.6637          4.2148
v  Velocity[Y]            -2.9423          3.0447       -0.096475        -0.29206
v  Velocity[Z]         -0.0014057       0.0015566      5.6888e-08      1.0626e-09
v  ǁVelocityǁ            0.028849          11.893          6.7298          4.2336
v  Pressure                1915.1           63543           43742           56340
v  Void Fraction       2.8643e-16         0.95055       0.0059175      0.00012055
v  k                    2.487e-17          1.4903         0.01473        0.021886
v  omega                    1e-24      1.9007e+08       1.047e+06           68671
v  scalar1                      0               0               0               0
v  TurbVisc            4.8126e-22         0.24348        0.013186          0.1256
v  CourantNb           0.00050121          4.4881         0.84348          0.1203
v  FourierNb            0.0060181         0.81545          0.1215        0.069821
v  total_pressure          1915.1           63543           43742           56340
v  Density Old             50.679            1000          994.26          999.88


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016386          4.7757         0.96498         0.19012


 TIME FOR THE TIME STEP               84:        0.14535E+01

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


 INSTANT    0.425000000E-03   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159339514E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18359E+01
   Friction velocity        uet   :  0.10926E+00 0.99544E+00
   Friction velocity        uk    :  0.10925E+00 0.14304E+01
   Dimensionless distance   yplus :  0.27011E+00 0.34560E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1122
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.2236E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43954E-01      22   0.45782E-04   0.28355E+01 0.16859E+03 
c  Velocity[X]                                      0.23542E+01 
c  Velocity[Y]                                      0.48126E+00 
c  Velocity[Z]                                      0.19023E-08 
c  Pressure     0.42105E-09    1802   0.15163E-02   0.60342E+00 0.26024E+03 
c  Void Fractio 0.36209E-08      36   0.56032E-08   0.13442E-01 0.69897E+04 
c  k            0.29582E-03      25   0.13523E-05   0.76886E-02 0.17051E+04 
c  omega        0.86189E+05      14   0.12020E-05   0.45282E+15 0.62873E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -1.271e-13                             4
a  omega              4.8119e-26                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9206          11.882          6.6603          4.2151
v  Velocity[Y]            -2.9529          3.0321       -0.096221         -0.2921
v  Velocity[Z]         -0.0013894       0.0015241      5.5133e-08      1.0282e-09
v  ǁVelocityǁ            0.008702          11.883           6.727          4.2339
v  Pressure                1886.1           63367           43607           56283
v  Void Fraction       2.3669e-16          0.9496       0.0060034      0.00012296
v  k                    2.744e-17          1.4849        0.014741        0.021887
v  omega                    1e-24      1.0166e+08      1.0453e+06           68622
v  scalar1                      0               0               0               0
v  TurbVisc            5.3181e-22         0.24348        0.013173         0.12557
v  CourantNb           0.00049834          4.4669         0.84319         0.12031
v  FourierNb            0.0060261         0.82231         0.12149        0.069719
v  total_pressure          1886.1           63367           43607           56283
v  Density Old             50.095            1000          994.17          999.88


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016392          4.7537         0.96468         0.19003


 TIME FOR THE TIME STEP               85:        0.15306E+01

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


 INSTANT    0.430000000E-03   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159353192E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18360E+01
   Friction velocity        uet   :  0.29591E-01 0.90758E+00
   Friction velocity        uk    :  0.29589E-01 0.14295E+01
   Dimensionless distance   yplus :  0.73214E-01 0.34539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1122
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.8302E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43959E-01      23   0.45013E-04   0.29327E+01 0.17144E+03 
c  Velocity[X]                                      0.24207E+01 
c  Velocity[Y]                                      0.51194E+00 
c  Velocity[Z]                                      0.19134E-08 
c  Pressure     0.11872E-08    1489   0.92015E-03   0.97284E+00 0.23927E+03 
c  Void Fractio 0.36772E-08      37   0.60150E-08   0.14149E-01 0.70845E+04 
c  k            0.29582E-03      24   0.17459E-06   0.56062E-03 0.46042E+03 
c  omega        0.86022E+05      13   0.53009E-06   0.90581E+14 0.28131E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.3545e-13                             4
a  omega              1.0311e-25                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9751          11.871           6.657          4.2154
v  Velocity[Y]            -2.9719          3.0238       -0.095968        -0.29214
v  Velocity[Z]         -0.0013691       0.0014916      5.1781e-08      9.6818e-10
v  ǁVelocityǁ            0.023307          11.874          6.7242          4.2343
v  Pressure                1887.7           63180           43483           56231
v  Void Fraction       1.9562e-16         0.95048       0.0060896      0.00012538
v  k                    3.023e-17          1.4758        0.014764        0.021888
v  omega                    1e-24      6.2802e+07      1.0446e+06           68591
v  scalar1                      0               0               0               0
v  TurbVisc            5.8676e-22         0.24349        0.013161         0.12554
v  CourantNb           0.00049548          4.4861         0.84292         0.12032
v  FourierNb            0.0060341         0.78393         0.12147        0.069618
v  total_pressure          1887.7           63180           43483           56231
v  Density Old             50.403            1000          994.09          999.88


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016398          4.7722         0.96439         0.18994


 TIME FOR THE TIME STEP               86:        0.13541E+01

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


 INSTANT    0.435000000E-03   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159366663E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18354E+01
   Friction velocity        uet   :  0.74724E-01 0.89872E+00
   Friction velocity        uk    :  0.74724E-01 0.14278E+01
   Dimensionless distance   yplus :  0.18488E+00 0.34498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1122
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.2426E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43964E-01      23   0.45611E-04   0.29445E+01 0.17177E+03 
c  Velocity[X]                                      0.24163E+01 
c  Velocity[Y]                                      0.52823E+00 
c  Velocity[Z]                                      0.17537E-08 
c  Pressure     0.11224E-08    1625   0.96277E-03   0.94180E+00 0.17560E+03 
c  Void Fractio 0.37337E-08      36   0.50232E-08   0.14824E-01 0.71653E+04 
c  k            0.29583E-03      25   0.31210E-06   0.72158E-03 0.52232E+03 
c  omega        0.86016E+05      13   0.17027E-06   0.11099E+14 0.98481E+03 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.4395e-13                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9943          11.861          6.6537          4.2157
v  Velocity[Y]            -2.9776          3.0312       -0.095722        -0.29218
v  Velocity[Z]         -0.0013542       0.0014585      5.1456e-08      9.7837e-10
v  ǁVelocityǁ            0.025516          11.864          6.7214          4.2346
v  Pressure                1915.3           63085           43399           56192
v  Void Fraction       1.6167e-16         0.95133       0.0061762      0.00012782
v  k                   3.3254e-17          1.4952         0.01479        0.021889
v  omega               2.3869e-23      5.4357e+07      1.0443e+06           68566
v  scalar1                      0               0               0               0
v  TurbVisc            6.4642e-22         0.24349         0.01315         0.12551
v  CourantNb           0.00049268          4.4792         0.84263         0.12033
v  FourierNb            0.0060422         0.80302         0.12146        0.069518
v  total_pressure          1915.3           63085           43399           56192
v  Density Old             51.348            1000             994          999.88


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016404          4.7642         0.96409         0.18985


 TIME FOR THE TIME STEP               87:        0.14274E+01

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


 INSTANT    0.440000000E-03   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159379961E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18352E+01
   Friction velocity        uet   :  0.10176E+00 0.11151E+01
   Friction velocity        uk    :  0.10176E+00 0.14272E+01
   Dimensionless distance   yplus :  0.25178E+00 0.34484E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1123
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.7743E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43969E-01      23   0.45555E-04   0.29654E+01 0.17236E+03 
c  Velocity[X]                                      0.24036E+01 
c  Velocity[Y]                                      0.56178E+00 
c  Velocity[Z]                                      0.16367E-08 
c  Pressure     0.24187E-09    1788   0.19478E-02   0.38026E+00 0.28040E+03 
c  Void Fractio 0.37896E-08      36   0.59561E-08   0.15022E-01 0.71292E+04 
c  k            0.29583E-03      24   0.11491E-05   0.49898E-02 0.13735E+04 
c  omega        0.82403E+12       2   0.21568E-11   0.19035E+16 0.12868E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.5254e-13                             4
a  omega               4.939e-25                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9926           11.85          6.6504           4.216
v  Velocity[Y]            -2.9932           3.044       -0.095461        -0.29222
v  Velocity[Z]         -0.0013488       0.0014343      4.8112e-08      8.9185e-10
v  ǁVelocityǁ            0.032668          11.854          6.7186          4.2349
v  Pressure                1802.6           62923           43258           56129
v  Void Fraction       1.3364e-16         0.95434       0.0062634      0.00013027
v  k                   3.6529e-17          1.5019        0.014812        0.021889
v  omega                    1e-24      1.8702e+08      1.0475e+06           68600
v  scalar1                      0               0               0               0
v  TurbVisc            7.1109e-22         0.24349        0.013138         0.12547
v  CourantNb           0.00048995          4.4831         0.84234         0.12034
v  FourierNb            0.0060504         0.82948         0.12145        0.069419
v  total_pressure          1802.6           62923           43258           56129
v  Density Old             50.471            1000          993.92          999.87


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01641          4.7669         0.96379         0.18976


 TIME FOR THE TIME STEP               88:        0.14958E+01

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


 INSTANT    0.445000000E-03   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159392965E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18345E+01
   Friction velocity        uet   :  0.10052E+00 0.99467E+00
   Friction velocity        uk    :  0.10052E+00 0.14270E+01
   Dimensionless distance   yplus :  0.24848E+00 0.34479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1123
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.7127E-14


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43974E-01      23   0.46366E-04   0.31010E+01 0.17624E+03 
c  Velocity[X]                                      0.25111E+01 
c  Velocity[Y]                                      0.58983E+00 
c  Velocity[Z]                                      0.14560E-08 
c  Pressure     0.33645E-08    1367   0.34352E-03   0.10327E+01 0.11420E+03 
c  Void Fractio 0.38429E-08      36   0.57192E-08   0.16345E-01 0.73520E+04 
c  k            0.29583E-03      24   0.13612E-05   0.68612E-02 0.16107E+04 
c  omega        0.86083E+05      12   0.12010E-05   0.43586E+15 0.61676E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.6119e-13                             4
a  omega              1.7464e-26                             1
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9853          11.838          6.6471          4.2163
v  Velocity[Y]             -2.995           3.037       -0.095204        -0.29226
v  Velocity[Z]         -0.0013367       0.0014165      4.6692e-08      8.7096e-10
v  ǁVelocityǁ            0.029761          11.841          6.7158          4.2352
v  Pressure                1916.1           62891           43208           56104
v  Void Fraction       1.1047e-16         0.95621       0.0063514      0.00013275
v  k                    4.007e-17          1.5092        0.014832         0.02189
v  omega                    1e-24      1.0023e+08      1.0457e+06           68552
v  scalar1                      0               0               0               0
v  TurbVisc            7.8112e-22          0.2435        0.013127         0.12544
v  CourantNb           0.00048722          4.4871         0.84205         0.12035
v  FourierNb            0.0060586         0.84079         0.12144        0.069324
v  total_pressure          1916.1           62891           43208           56104
v  Density Old             49.623            1000          993.83          999.87


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016416          4.7697          0.9635         0.18968


 TIME FOR THE TIME STEP               89:        0.12864E+01

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


 INSTANT    0.450000000E-03   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159405869E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18341E+01
   Friction velocity        uet   :  0.11430E+00 0.90834E+00
   Friction velocity        uk    :  0.11429E+00 0.14268E+01
   Dimensionless distance   yplus :  0.28251E+00 0.34473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1123
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1788E-14


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43978E-01      23   0.46273E-04   0.30336E+01 0.17430E+03 
c  Velocity[X]                                      0.24383E+01 
c  Velocity[Y]                                      0.59531E+00 
c  Velocity[Z]                                      0.12465E-08 
c  Pressure     0.19982E-09    1752   0.19952E-02   0.32023E+00 0.28724E+03 
c  Void Fractio 0.38980E-08      37   0.63233E-08   0.17126E-01 0.74412E+04 
c  k            0.29583E-03      24   0.26508E-06   0.50685E-03 0.43775E+03 
c  omega        0.17147E+13       2   0.12003E-12   0.84936E+14 0.27236E+04 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.6983e-13                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.973          11.822          6.6438          4.2166
v  Velocity[Y]            -3.0123          3.0346       -0.094954         -0.2923
v  Velocity[Z]         -0.0013235       0.0014285      4.5768e-08      8.5345e-10
v  ǁVelocityǁ            0.015764          11.828           6.713          4.2355
v  Pressure                1916.6           62730           43064           56039
v  Void Fraction       9.1324e-17         0.95954       0.0064403      0.00013523
v  k                   4.3895e-17          1.5047         0.01486        0.021891
v  omega               1.6746e-19      6.2233e+07      1.0449e+06           68522
v  scalar1                      0               0               0               0
v  TurbVisc            8.5684e-22          0.2435        0.013116         0.12541
v  CourantNb            0.0004845          4.4722         0.84176         0.12036
v  FourierNb            0.0060668         0.87953         0.12143        0.069227
v  total_pressure          1916.6           62730           43064           56039
v  Density Old              46.61            1000          993.74          999.87


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016422          4.7539          0.9632         0.18959


 TIME FOR THE TIME STEP               90:        0.15021E+01

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


 INSTANT    0.455000000E-03   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159418469E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18337E+01
   Friction velocity        uet   :  0.68625E-01 0.89211E+00
   Friction velocity        uk    :  0.68621E-01 0.14265E+01
   Dimensionless distance   yplus :  0.16979E+00 0.34467E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1123
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1024E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43983E-01      22   0.45469E-04   0.31048E+01 0.17632E+03 
c  Velocity[X]                                      0.24924E+01 
c  Velocity[Y]                                      0.61245E+00 
c  Velocity[Z]                                      0.13752E-08 
c  Pressure     0.54417E-09    1526   0.16243E-02   0.71518E+00 0.20681E+03 
c  Void Fractio 0.39504E-08      37   0.66648E-08   0.17012E-01 0.73353E+04 
c  k            0.29583E-03      24   0.32184E-06   0.68617E-03 0.50931E+03 
c  omega        0.86016E+05      13   0.16344E-06   0.10043E+14 0.93659E+03 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.7839e-13                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9707          11.804          6.6406          4.2169
v  Velocity[Y]            -3.0161          3.0317       -0.094701        -0.29234
v  Velocity[Z]          -0.001347       0.0014263      4.4662e-08      8.3176e-10
v  ǁVelocityǁ            0.023422          11.813          6.7102          4.2358
v  Pressure                1875.4           62633           42964           55993
v  Void Fraction       7.5503e-17         0.96175         0.00653      0.00013774
v  k                   4.8022e-17          1.4895        0.014889        0.021892
v  omega               3.7275e-21      5.8411e+07      1.0447e+06           68501
v  scalar1                      0               0               0               0
v  TurbVisc            9.3863e-22          0.2435        0.013105         0.12538
v  CourantNb           0.00048182           4.472         0.84146         0.12037
v  FourierNb             0.006075         0.87453         0.12143        0.069133
v  total_pressure          1875.4           62633           42964           55993
v  Density Old             44.744            1000          993.65          999.87


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016428          4.7527         0.96289         0.18951


 TIME FOR THE TIME STEP               91:        0.13792E+01

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


 INSTANT    0.460000000E-03   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159430858E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18337E+01
   Friction velocity        uet   :  0.10874E+00 0.11207E+01
   Friction velocity        uk    :  0.10873E+00 0.14242E+01
   Dimensionless distance   yplus :  0.26906E+00 0.34410E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1124
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1128E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43988E-01      22   0.44866E-04   0.30866E+01 0.17579E+03 
c  Velocity[X]                                      0.24528E+01 
c  Velocity[Y]                                      0.63383E+00 
c  Velocity[Z]                                      0.98057E-09 
c  Pressure     0.13276E-08    1616   0.86369E-03   0.96056E+00 0.32176E+03 
c  Void Fractio 0.40033E-08      37   0.51817E-08   0.17974E-01 0.74588E+04 
c  k            0.29583E-03      24   0.11676E-05   0.53412E-02 0.14210E+04 
c  omega        0.99125E+05      12   0.22123E-05   0.19168E+16 0.12911E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -1.868e-13                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9737          11.785          6.6373          4.2172
v  Velocity[Y]            -3.0396          3.0284       -0.094469        -0.29238
v  Velocity[Z]         -0.0013344        0.001422      4.4369e-08      8.3295e-10
v  ǁVelocityǁ           0.0098712          11.795          6.7074          4.2361
v  Pressure                1917.1           62442           42803           55920
v  Void Fraction       6.2431e-17         0.96296       0.0066204      0.00014026
v  k                   5.2469e-17           1.481        0.014912        0.021893
v  omega               8.1307e-23      1.8771e+08      1.0483e+06           68542
v  scalar1                      0               0               0               0
v  TurbVisc            1.0269e-21          0.2435        0.013094         0.12535
v  CourantNb           0.00047924          4.4751         0.84116         0.12038
v  FourierNb            0.0060832         0.87393         0.12142        0.069036
v  total_pressure          1917.1           62442           42803           55920
v  Density Old             41.419            1000          993.57          999.86


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016434          4.7552         0.96258         0.18942


 TIME FOR THE TIME STEP               92:        0.14212E+01

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


 INSTANT    0.465000000E-03   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159442908E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18332E+01
   Friction velocity        uet   :  0.51583E-01 0.99969E+00
   Friction velocity        uk    :  0.51580E-01 0.14234E+01
   Dimensionless distance   yplus :  0.12762E+00 0.34392E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1124
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2790E-15


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43992E-01      23   0.47045E-04   0.29999E+01 0.17329E+03 
c  Velocity[X]                                      0.23553E+01 
c  Velocity[Y]                                      0.64457E+00 
c  Velocity[Z]                                      0.13582E-08 
c  Pressure     0.90396E-09    1787   0.12253E-02   0.87541E+00 0.43384E+03 
c  Void Fractio 0.40556E-08      36   0.62935E-08   0.17820E-01 0.73487E+04 
c  k            0.29584E-03      24   0.13810E-05   0.78754E-02 0.17256E+04 
c  omega        0.22520E+08      21   0.20019E-02   0.11468E+29 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.9499e-13                             4
a  omega        
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.954          11.768          6.6341          4.2174
v  Velocity[Y]            -3.0477           3.024       -0.094214        -0.29241
v  Velocity[Z]         -0.0013403       0.0014157      4.2909e-08      8.1085e-10
v  ǁVelocityǁ            0.019813           11.78          6.7046          4.2364
v  Pressure                1363.6           62148           42585           55823
v  Void Fraction       5.1634e-17         0.96352       0.0067119       0.0001428
v  k                   5.7255e-17          1.5085        0.014931        0.021894
v  omega               1.8444e-24      3.9032e+14      9.0445e+09       1.902e+08
v  scalar1                      0               0               0               0
v  TurbVisc             1.122e-21         0.24351        0.013083         0.12532
v  CourantNb           0.00047666          4.4663         0.84083         0.12039
v  FourierNb            0.0060916         0.88517         0.12141        0.068941
v  total_pressure          1363.6           62148           42585           55823
v  Density Old             39.209            1000          993.48          999.86


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01644          4.7453         0.96224         0.18933


 TIME FOR THE TIME STEP               93:        0.15056E+01

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


 INSTANT    0.470000000E-03   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159454497E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18326E+01
   Friction velocity        uet   :  0.11716E+00 0.91255E+00
   Friction velocity        uk    :  0.11716E+00 0.14215E+01
   Dimensionless distance   yplus :  0.29291E+00 0.34347E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1124
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.4670E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43997E-01      23   0.47016E-04   0.30810E+01 0.17560E+03 
c  Velocity[X]                                      0.24184E+01 
c  Velocity[Y]                                      0.66264E+00 
c  Velocity[Z]                                      0.88301E-09 
c  Pressure     0.10725E-07    1191   0.11214E-03   0.10110E+01 0.19695E+03 
c  Void Fractio 0.41060E-08      36   0.59184E-08   0.18657E-01 0.74409E+04 
c  k            0.29584E-03      24   0.18321E-06   0.78491E-03 0.54474E+03 
c  omega        0.17923E+22       2   0.14692E-15   0.28671E+28 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.0285e-13                             4
a  omega             -4.2868e+06                             5
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9257           11.75          6.6309          4.2177
v  Velocity[Y]            -3.0697           3.032       -0.093973        -0.29245
v  Velocity[Z]         -0.0013269       0.0014372      4.2355e-08      8.0279e-10
v  ǁVelocityǁ            0.018488          11.762          6.7018          4.2367
v  Pressure                1917.6           62089           42496           55779
v  Void Fraction       4.2705e-17         0.96515       0.0068042      0.00014535
v  k                   6.2402e-17          1.5097        0.014954        0.021895
v  omega                1.295e-24      1.9516e+14      4.5631e+09      9.6025e+07
v  scalar1                      0               0               0               0
v  TurbVisc            1.2243e-21         0.24351        0.013072         0.12529
v  CourantNb           0.00047418           4.468         0.84049          0.1204
v  FourierNb               0.0061         0.89569         0.12141        0.068847
v  total_pressure          1917.6           62089           42496           55779
v  Density Old                 38            1000          993.39          999.86


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016446          4.7458          0.9619         0.18925


 TIME FOR THE TIME STEP               94:        0.12013E+01

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


 INSTANT    0.475000000E-03   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159465874E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18319E+01
   Friction velocity        uet   :  0.90397E-01 0.87605E+00
   Friction velocity        uk    :  0.90390E-01 0.14221E+01
   Dimensionless distance   yplus :  0.22365E+00 0.34360E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1124
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.5383E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44001E-01      22   0.46401E-04   0.29498E+01 0.17181E+03 
c  Velocity[X]                                      0.23007E+01 
c  Velocity[Y]                                      0.64910E+00 
c  Velocity[Z]                                      0.62067E-09 
c  Pressure     0.13308E-09    1788   0.20710E-02   0.21381E+00 0.42512E+03 
c  Void Fractio 0.41569E-08      37   0.62937E-08   0.17969E-01 0.72277E+04 
c  k            0.29584E-03      24   0.32174E-06   0.75035E-03 0.53258E+03 
c  omega        0.69194E+20       2   0.21656E-15   0.71678E+27 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.7097e-10                             7
a  omega             -1.1695e+11                             6
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8825          11.727          6.6276           4.218
v  Velocity[Y]            -3.0741          3.0341       -0.093708        -0.29249
v  Velocity[Z]         -0.0013588       0.0014445       4.105e-08       7.691e-10
v  ǁVelocityǁ            0.017437          11.742          6.6991          4.2369
v  Pressure                1587.1           61844           42283           55684
v  Void Fraction       3.5328e-17         0.96591       0.0068976      0.00014791
v  k                   1.3809e-18          1.5031        0.014983        0.021896
v  omega                    1e-24       9.758e+13      2.2846e+09      4.8099e+07
v  scalar1                      0               0               0               0
v  TurbVisc            5.5461e-27         0.24351        0.013062         0.12526
v  CourantNb           0.00047166          4.4442         0.84017         0.12041
v  FourierNb            0.0061085         0.88893         0.12141        0.068756
v  total_pressure          1587.1           61844           42283           55684
v  Density Old             37.442            1000          993.29          999.86


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016452           4.721         0.96158         0.18917


 TIME FOR THE TIME STEP               95:        0.15036E+01

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


 INSTANT    0.480000000E-03   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159476798E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18315E+01
   Friction velocity        uet   :  0.10937E+00 0.87059E+00
   Friction velocity        uk    :  0.10937E+00 0.14193E+01
   Dimensionless distance   yplus :  0.27075E+00 0.34292E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1124
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.9244E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44005E-01      22   0.45372E-04   0.29697E+01 0.17237E+03 
c  Velocity[X]                                      0.23068E+01 
c  Velocity[Y]                                      0.66292E+00 
c  Velocity[Z]                                      0.51429E-09 
c  Pressure     0.68349E-08    1266   0.17630E-03   0.10154E+01 0.41851E+03 
c  Void Fractio 0.42062E-08      37   0.52110E-08   0.18801E-01 0.73184E+04 
c  k            0.29584E-03      24   0.27690E-06   0.76897E-03 0.53913E+03 
c  omega        0.32199E+20       2   0.24092E-15   0.17919E+27 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.9647e-09                            18
a  omega               -5.99e+06                             2
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.834          11.705          6.6243          4.2182
v  Velocity[Y]            -3.0909          3.0194       -0.093453        -0.29252
v  Velocity[Z]         -0.0013615       0.0014202      4.1474e-08      7.8429e-10
v  ǁVelocityǁ            0.015398          11.721          6.6963          4.2372
v  Pressure                  1848           61591           42074           55589
v  Void Fraction       2.9229e-17          0.9661        0.006992      0.00015049
v  k                   9.0712e-22          1.4795        0.015014        0.021897
v  omega               5.9975e-23       4.879e+13      1.1429e+09      2.4084e+07
v  scalar1                      0               0               0               0
v  TurbVisc            1.5136e-31         0.24352        0.013052         0.12523
v  CourantNb           0.00046924          4.4456         0.83984         0.12042
v  FourierNb            0.0061169          0.8692         0.12141        0.068666
v  total_pressure            1848           61591           42074           55589
v  Density Old             35.815            1000           993.2          999.85


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016458          4.7215         0.96126         0.18909


 TIME FOR THE TIME STEP               96:        0.12205E+01

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


 INSTANT    0.485000000E-03   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159487274E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18309E+01
   Friction velocity        uet   :  0.54778E-01 0.11236E+01
   Friction velocity        uk    :  0.54778E-01 0.14176E+01
   Dimensionless distance   yplus :  0.13549E+00 0.34251E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1125
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1811E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44009E-01      23   0.45803E-04   0.29441E+01 0.17161E+03 
c  Velocity[X]                                      0.23219E+01 
c  Velocity[Y]                                      0.62221E+00 
c  Velocity[Z]                                      0.24287E-09 
c  Pressure     0.17224E-08    1652   0.70607E-03   0.99786E+00 0.40598E+03 
c  Void Fractio 0.42569E-08      37   0.55751E-08   0.19157E-01 0.73128E+04 
c  k            0.29584E-03      24   0.13550E-05   0.67195E-02 0.15937E+04 
c  omega        0.11935E+16       2   0.28680E-11   0.44798E+26 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -5.2396e-09                            20
a  omega             -3.4457e+07                             5
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8063           11.68           6.621          4.2184
v  Velocity[Y]            -3.0955           3.002       -0.093195        -0.29256
v  Velocity[Z]         -0.0013497       0.0014311       4.053e-08      7.6256e-10
v  ǁVelocityǁ            0.017184          11.697          6.6935          4.2374
v  Pressure                1876.6           61333           41870           55499
v  Void Fraction       2.4189e-17         0.96663       0.0070874      0.00015308
v  k                   1.5987e-22          1.4664         0.01504        0.021898
v  omega               4.2701e-24      2.4395e+13      5.7197e+08      1.2077e+07
v  scalar1                      0               0               0               0
v  TurbVisc            8.2948e-34         0.24352        0.013042          0.1252
v  CourantNb           0.00046684           4.463         0.83951         0.12043
v  FourierNb            0.0061254         0.86008         0.12142        0.068576
v  total_pressure          1876.6           61333           41870           55499
v  Density Old             35.053            1000          993.11          999.85


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016464          4.7385         0.96093         0.18901


 TIME FOR THE TIME STEP               97:        0.14160E+01

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


 INSTANT    0.490000000E-03   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159497324E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18303E+01
   Friction velocity        uet   :  0.10551E+00 0.10043E+01
   Friction velocity        uk    :  0.10551E+00 0.14160E+01
   Dimensionless distance   yplus :  0.26377E+00 0.34213E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1125
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2201E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44013E-01      23   0.46795E-04   0.28603E+01 0.16914E+03 
c  Velocity[X]                                      0.22306E+01 
c  Velocity[Y]                                      0.62971E+00 
c  Velocity[Z]                                      0.45069E-09 
c  Pressure     0.16264E-08    1578   0.77758E-03   0.99208E+00 0.38978E+03 
c  Void Fractio 0.43041E-08      36   0.54398E-08   0.17427E-01 0.69057E+04 
c  k            0.29585E-03      24   0.15109E-05   0.80990E-02 0.17497E+04 
c  omega        0.55683E+16       2   0.31758E-12   0.11200E+26 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.1918e-09                            19
a  omega              -6.947e+05                             5
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.779          11.654          6.6176          4.2187
v  Velocity[Y]            -3.1098          2.9952        -0.09293        -0.29259
v  Velocity[Z]         -0.0013563        0.001449      4.0734e-08      7.7003e-10
v  ǁVelocityǁ            0.014511          11.673          6.6907          4.2377
v  Pressure                1915.5           61137           41680           55411
v  Void Fraction       2.0021e-17         0.96743       0.0071837      0.00015569
v  k                   3.4414e-24          1.4854        0.015065        0.021899
v  omega               2.6508e-19      1.2198e+13      2.8651e+08      6.0726e+06
v  scalar1                      0               0               0               0
v  TurbVisc            7.0104e-35         0.24352        0.013033         0.12517
v  CourantNb           0.00046446          4.4677         0.83918         0.12044
v  FourierNb             0.006134         0.85387         0.12142        0.068489
v  total_pressure          1915.5           61137           41680           55411
v  Density Old             34.863            1000          993.02          999.85


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01647          4.7423          0.9606         0.18893


 TIME FOR THE TIME STEP               98:        0.13794E+01

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


 INSTANT    0.495000000E-03   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159506947E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18293E+01
   Friction velocity        uet   :  0.66321E-01 0.91563E+00
   Friction velocity        uk    :  0.66315E-01 0.14152E+01
   Dimensionless distance   yplus :  0.16408E+00 0.34193E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1125
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1938E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44017E-01      23   0.46862E-04   0.28894E+01 0.16999E+03 
c  Velocity[X]                                      0.22878E+01 
c  Velocity[Y]                                      0.60153E+00 
c  Velocity[Z]                                      0.34411E-09 
c  Pressure     0.89139E-09    1787   0.11436E-02   0.89113E+00 0.34924E+03 
c  Void Fractio 0.43523E-08      37   0.48378E-08   0.16729E-01 0.66993E+04 
c  k            0.29585E-03      23   0.34854E-06   0.66214E-03 0.50027E+03 
c  omega        0.32236E+13       3   0.28170E-09   0.27999E+25 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -6.4565e-10                            17
a  omega             -1.0354e+07                             5
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7427          11.629          6.6143          4.2189
v  Velocity[Y]            -3.1098          3.0096       -0.092662        -0.29262
v  Velocity[Z]         -0.0013669       0.0014674      3.9999e-08      7.5143e-10
v  ǁVelocityǁ            0.016065          11.651           6.688          4.2379
v  Pressure                1918.6           60963           41508           55332
v  Void Fraction       1.6573e-17         0.96915       0.0072809       0.0001583
v  k                        1e-24          1.4793          0.0151        0.021901
v  omega               1.7241e-20      6.0988e+12      1.4378e+08      3.0705e+06
v  scalar1                      0               0               0               0
v  TurbVisc            3.0187e-36         0.24353        0.013023         0.12515
v  CourantNb           0.00046213          4.4551         0.83882         0.12045
v  FourierNb            0.0061429         0.84712         0.12142        0.068402
v  total_pressure          1918.6           60963           41508           55332
v  Density Old             34.334            1000          992.92          999.85


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016477          4.7285         0.96024         0.18885


 TIME FOR THE TIME STEP               99:        0.14948E+01

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


 INSTANT    0.500000000E-03   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159516194E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18281E+01
   Friction velocity        uet   :  0.91330E-01 0.87937E+00
   Friction velocity        uk    :  0.91321E-01 0.14137E+01
   Dimensionless distance   yplus :  0.22597E+00 0.34156E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1125
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1807E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44021E-01      22   0.45308E-04   0.28303E+01 0.16823E+03 
c  Velocity[X]                                      0.22471E+01 
c  Velocity[Y]                                      0.58322E+00 
c  Velocity[Z]                                      0.29632E-09 
c  Pressure     0.22114E-09    1782   0.19267E-02   0.35427E+00 0.38922E+03 
c  Void Fractio 0.43994E-08      37   0.59172E-08   0.14996E-01 0.62811E+04 
c  k            0.29585E-03      24   0.34374E-06   0.65961E-03 0.49927E+03 
c  omega        0.82525E+12       3   0.56021E-09   0.69998E+24 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -4.5073e-10                            14
a  omega                  -50819                             3
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6931          11.622          6.6109          4.2191
v  Velocity[Y]            -3.1006          3.0068       -0.092388        -0.29265
v  Velocity[Z]         -0.0013688       0.0014431      3.9981e-08      7.5457e-10
v  ǁVelocityǁ            0.020092          11.645          6.6852          4.2381
v  Pressure                1778.6           60750           41317           55244
v  Void Fraction       1.3721e-17         0.97001       0.0073789      0.00016093
v  k                   6.9093e-23          1.4761        0.015139        0.021902
v  omega               2.6466e-22      3.0494e+12      7.2416e+07      1.5695e+06
v  scalar1                      0               0               0               0
v  TurbVisc            1.7548e-36         0.24353        0.013013         0.12512
v  CourantNb           0.00045984          4.4421         0.83847         0.12045
v  FourierNb            0.0061517         0.84261         0.12143        0.068314
v  total_pressure          1778.6           60750           41317           55244
v  Density Old             33.538            1000          992.82          999.84


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016483          4.7148         0.95991         0.18877


 TIME FOR THE TIME STEP              100:        0.15029E+01

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


 INSTANT    0.505000000E-03   TIME STEP NUMBER             101
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159525013E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18271E+01
   Friction velocity        uet   :  0.94130E-01 0.85754E+00
   Friction velocity        uk    :  0.94129E-01 0.14114E+01
   Dimensionless distance   yplus :  0.23532E+00 0.34101E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1125
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.3404E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44024E-01      22   0.46130E-04   0.29089E+01 0.17054E+03 
c  Velocity[X]                                      0.23210E+01 
c  Velocity[Y]                                      0.58789E+00 
c  Velocity[Z]                                      0.45959E-09 
c  Pressure     0.33511E-08    1320   0.33427E-03   0.10133E+01 0.38938E+03 
c  Void Fractio 0.44470E-08      37   0.51279E-08   0.14626E-01 0.61431E+04 
c  k            0.29585E-03      23   0.29418E-06   0.61321E-03 0.48135E+03 
c  omega        0.20985E+12       3   0.11105E-08   0.17499E+24 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.1663e-10                            13
a  omega                  -44421                             3
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6422          11.621          6.6075          4.2193
v  Velocity[Y]            -3.1197          2.9933       -0.092113        -0.29268
v  Velocity[Z]         -0.0013711       0.0014236      4.0013e-08      7.6148e-10
v  ǁVelocityǁ            0.014537          11.636          6.6824          4.2383
v  Pressure                1919.2           60517           41123           55159
v  Void Fraction       1.1362e-17         0.97032       0.0074775      0.00016357
v  k                    4.625e-21          1.4573        0.015179        0.021903
v  omega               3.9953e-24      1.5247e+12      3.6733e+07      8.1899e+05
v  scalar1                      0               0               0               0
v  TurbVisc            2.4256e-34         0.24353        0.013004         0.12509
v  CourantNb           0.00045754          4.4359         0.83811         0.12046
v  FourierNb            0.0061606          0.8333         0.12144        0.068228
v  total_pressure          1919.2           60517           41123           55159
v  Density Old              31.82            1000          992.73          999.84


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01649          4.7082         0.95955         0.18869


 TIME FOR THE TIME STEP              101:        0.12557E+01

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


 INSTANT    0.510000000E-03   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159533433E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18262E+01
   Friction velocity        uet   :  0.63632E-01 0.84249E+00
   Friction velocity        uk    :  0.63625E-01 0.14081E+01
   Dimensionless distance   yplus :  0.15744E+00 0.34021E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1125
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2289E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44028E-01      23   0.46668E-04   0.29081E+01 0.17050E+03 
c  Velocity[X]                                      0.23394E+01 
c  Velocity[Y]                                      0.56871E+00 
c  Velocity[Z]                                      0.20141E-09 
c  Pressure     0.39974E-09    1842   0.16372E-02   0.58261E+00 0.42025E+03 
c  Void Fractio 0.44948E-08      37   0.62944E-08   0.14371E-01 0.60306E+04 
c  k            0.29585E-03      23   0.16538E-06   0.38993E-03 0.38380E+03 
c  omega        0.52150E+11       3   0.22287E-08   0.43748E+23 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.8183e-10                            12
a  omega             -4.2436e+05                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6175          11.611           6.604          4.2194
v  Velocity[Y]            -3.1099          2.9933       -0.091837        -0.29271
v  Velocity[Z]         -0.0013711       0.0014472      3.9691e-08      7.5311e-10
v  ǁVelocityǁ            0.018407          11.629          6.6797          4.2385
v  Pressure                1919.1           60267           40914           55065
v  Void Fraction       9.4108e-18         0.97034       0.0075767      0.00016622
v  k                   1.7215e-19           1.441         0.01522        0.021905
v  omega                    1e-24      7.6235e+11      1.8891e+07      4.4371e+05
v  scalar1                      0               0               0               0
v  TurbVisc            3.2481e-32         0.24354        0.012994         0.12506
v  CourantNb           0.00045529          4.4445         0.83776         0.12047
v  FourierNb            0.0061696         0.85516         0.12146        0.068144
v  total_pressure          1919.1           60267           40914           55065
v  Density Old              30.96            1000          992.63          999.84


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016496          4.7163         0.95921         0.18861


 TIME FOR THE TIME STEP              102:        0.15229E+01

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


 INSTANT    0.515000000E-03   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159541406E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18250E+01
   Friction velocity        uet   :  0.85772E-01 0.11364E+01
   Friction velocity        uk    :  0.85772E-01 0.14062E+01
   Dimensionless distance   yplus :  0.21443E+00 0.33976E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.3367E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44031E-01      23   0.46057E-04   0.29240E+01 0.17096E+03 
c  Velocity[X]                                      0.23769E+01 
c  Velocity[Y]                                      0.54710E+00 
c  Velocity[Z]                                      0.19616E-09 
c  Pressure     0.18519E-09    1752   0.19124E-02   0.30846E+00 0.31419E+03 
c  Void Fractio 0.45422E-08      36   0.65161E-08   0.13099E-01 0.57024E+04 
c  k            0.29585E-03      23   0.14958E-05   0.79496E-02 0.17329E+04 
c  omega        0.12639E+11       3   0.45383E-08   0.10937E+23 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                  -1.033e-11                            10
a  omega             -2.0851e+05                             5
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5905          11.603          6.6006          4.2196
v  Velocity[Y]            -3.1134           2.994       -0.091569        -0.29274
v  Velocity[Z]         -0.0013786       0.0014598      3.9856e-08       7.597e-10
v  ǁVelocityǁ              0.0112          11.624          6.6769          4.2387
v  Pressure                1817.6           60111           40763           54995
v  Void Fraction       7.7952e-18         0.97042       0.0076764      0.00016888
v  k                   4.6103e-18          1.4735        0.015257        0.021906
v  omega                    1e-24      3.8117e+11       9.974e+06      2.5612e+05
v  scalar1                      0               0               0               0
v  TurbVisc            2.4184e-30         0.24354        0.012985         0.12504
v  CourantNb            0.0004532          4.4451         0.83741         0.12048
v  FourierNb            0.0061787         0.85023         0.12148        0.068061
v  total_pressure          1817.6           60111           40763           54995
v  Density Old              30.65            1000          992.53          999.84


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016503          4.7161         0.95889         0.18854


 TIME FOR THE TIME STEP              103:        0.14800E+01

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


 INSTANT    0.520000000E-03   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159549037E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18241E+01
   Friction velocity        uet   :  0.29461E-01 0.10178E+01
   Friction velocity        uk    :  0.29457E-01 0.14037E+01
   Dimensionless distance   yplus :  0.72714E-01 0.33915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.3873E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44034E-01      22   0.46339E-04   0.29490E+01 0.17168E+03 
c  Velocity[X]                                      0.23761E+01 
c  Velocity[Y]                                      0.57289E+00 
c  Velocity[Z]                                      0.22547E-09 
c  Pressure     0.20960E-08    1418   0.54712E-03   0.10136E+01 0.25753E+03 
c  Void Fractio 0.45902E-08      36   0.49407E-08   0.12850E-01 0.55937E+04 
c  k            0.29586E-03      23   0.16044E-05   0.99716E-02 0.19409E+04 
c  omega        0.30387E+10       3   0.92203E-08   0.27343E+22 0.19998E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.1269e-11                             8
a  omega                  -82806                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5522            11.6          6.5971          4.2198
v  Velocity[Y]            -3.1259          2.9886       -0.091291        -0.29277
v  Velocity[Z]         -0.0013793       0.0014547      3.9701e-08      7.5694e-10
v  ǁVelocityǁ           0.0055298          11.613          6.6741          4.2389
v  Pressure                1919.4           59997           40639           54937
v  Void Fraction       6.4576e-18         0.97037       0.0077765      0.00017155
v  k                   9.5054e-17          1.4597        0.015289        0.021907
v  omega                    1e-24      1.9059e+11      5.5112e+06      1.6225e+05
v  scalar1                      0               0               0               0
v  TurbVisc            1.2952e-28         0.24354        0.012977         0.12501
v  CourantNb           0.00045097          4.4296         0.83706         0.12048
v  FourierNb            0.0061876         0.84789         0.12149        0.067979
v  total_pressure          1919.4           59997           40639           54937
v  Density Old             30.631            1000          992.43          999.83


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016509          4.6994         0.95855         0.18846


 TIME FOR THE TIME STEP              104:        0.13436E+01

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


 INSTANT    0.525000000E-03   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159556393E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18229E+01
   Friction velocity        uet   :  0.31572E-01 0.92830E+00
   Friction velocity        uk    :  0.31572E-01 0.14015E+01
   Dimensionless distance   yplus :  0.78086E-01 0.33862E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.2202E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44038E-01      24   0.46493E-04   0.28826E+01 0.16972E+03 
c  Velocity[X]                                      0.23385E+01 
c  Velocity[Y]                                      0.54410E+00 
c  Velocity[Z]                                      0.26212E-09 
c  Pressure     0.22810E-09    1662   0.18882E-02   0.37423E+00 0.19910E+03 
c  Void Fractio 0.46381E-08      37   0.52102E-08   0.12403E-01 0.54432E+04 
c  k            0.29586E-03      22   0.22171E-06   0.52442E-03 0.44507E+03 
c  omega        0.72338E+09      15   0.24645E-06   0.15488E+23 0.20000E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.7227e-11                             7
a  omega                  -24470                             4
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5084          11.596          6.5937            4.22
v  Velocity[Y]            -3.1321          2.9867        -0.09103         -0.2928
v  Velocity[Z]         -0.0013767       0.0014379      3.9877e-08      7.6304e-10
v  ǁVelocityǁ           0.0088169           11.61          6.6714          4.2391
v  Pressure                1902.2           59934           40550           54893
v  Void Fraction       5.3497e-18         0.97012       0.0078767      0.00017423
v  k                    1.495e-16          1.4511        0.015333        0.021909
v  omega                    1e-24      5.2872e+11      1.5891e+07      2.9913e+05
v  scalar1                      0               0               0               0
v  TurbVisc            5.3392e-27         0.24355        0.012968         0.12499
v  CourantNb           0.00044886          4.4312          0.8367         0.12049
v  FourierNb            0.0061967         0.84932         0.12151        0.067896
v  total_pressure          1902.2           59934           40550           54893
v  Density Old             30.555            1000          992.33          999.83


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016516             4.7          0.9582         0.18839


 TIME FOR THE TIME STEP              105:        0.14983E+01

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


 INSTANT    0.530000000E-03   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159563531E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18215E+01
   Friction velocity        uet   :  0.32868E-01 0.89293E+00
   Friction velocity        uk    :  0.32864E-01 0.14004E+01
   Dimensionless distance   yplus :  0.81319E-01 0.33835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.1585E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44041E-01      23   0.45262E-04   0.30163E+01 0.17360E+03 
c  Velocity[X]                                      0.24694E+01 
c  Velocity[Y]                                      0.54692E+00 
c  Velocity[Z]                                      0.41842E-09 
c  Pressure     0.11315E-08    1508   0.90031E-03   0.95974E+00 0.20316E+03 
c  Void Fractio 0.46876E-08      37   0.50654E-08   0.13559E-01 0.56369E+04 
c  k            0.29586E-03      26   0.36999E-06   0.58374E-02 0.14848E+04 
c  omega        0.12992E+11       3   0.69170E-08   0.38720E+22 0.19999E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -9.1617e-08                             6
a  omega             -1.8171e+06                             6
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4948          11.599          6.5903          4.2201
v  Velocity[Y]            -3.1433            2.98       -0.090765        -0.29283
v  Velocity[Z]         -0.0013845       0.0014666      4.0021e-08      7.6703e-10
v  ǁVelocityǁ          0.00035868          11.611          6.6687          4.2393
v  Pressure                  1920           59801           40449           54850
v  Void Fraction       4.4323e-18         0.96999       0.0079769      0.00017691
v  k                   1.6092e-16          1.4442        0.015343         0.02191
v  omega                    1e-24      2.6436e+11      8.4811e+06      1.8399e+05
v  scalar1                      0               0               0               0
v  TurbVisc            1.7377e-25         0.24355        0.012959         0.12496
v  CourantNb           0.00044672          4.4043         0.83634          0.1205
v  FourierNb            0.0062058         0.84957         0.12152        0.067815
v  total_pressure            1920           59801           40449           54850
v  Density Old             30.597            1000          992.23          999.83


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016522          4.6735         0.95786         0.18831


 TIME FOR THE TIME STEP              106:        0.13947E+01

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


 INSTANT    0.535000000E-03   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159570479E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18202E+01
   Friction velocity        uet   :  0.56160E-02 0.87233E+00
   Friction velocity        uk    :  0.56160E-02 0.13986E+01
   Dimensionless distance   yplus :  0.13905E-01 0.33792E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget:  0.5263E-14


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44044E-01      23   0.46012E-04   0.29064E+01 0.17040E+03 
c  Velocity[X]                                      0.23340E+01 
c  Velocity[Y]                                      0.57246E+00 
c  Velocity[Z]                                      0.27880E-09 
c  Pressure     0.14154E-09    1969   0.25559E-02   0.24462E+00 0.32517E+03 
c  Void Fractio 0.47364E-08      38   0.51370E-08   0.99067E-02 0.47723E+04 
c  k            0.29586E-03      24   0.30652E-06   0.91188E-03 0.58678E+03 
c  omega        0.32707E+10       3   0.13745E-07   0.96799E+21 0.19994E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.4971e-06                             7
a  omega              -1.397e+07                             9
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4833          11.622          6.5869          4.2203
v  Velocity[Y]            -3.1453          2.9714       -0.090538        -0.29286
v  Velocity[Z]          -0.001396       0.0014799      4.0027e-08       7.676e-10
v  ǁVelocityǁ           0.0040941          11.632          6.6659          4.2395
v  Pressure                1920.3           60052           40601           54907
v  Void Fraction       3.6715e-18         0.96991       0.0080759      0.00017961
v  k                   1.7305e-16          1.4274        0.015384        0.021911
v  omega                    1e-24      1.3218e+11      4.7682e+06      1.2624e+05
v  scalar1                      0               0               0               0
v  TurbVisc            4.6965e-24         0.24355         0.01295         0.12493
v  CourantNb            0.0004445           4.397         0.83602         0.12051
v  FourierNb             0.006215         0.84943         0.12154        0.067735
v  total_pressure          1920.3           60052           40601           54907
v  Density Old             30.855            1000          992.13          999.83


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016529          4.6659         0.95756         0.18824


 TIME FOR THE TIME STEP              107:        0.16515E+01

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


 INSTANT    0.540000000E-03   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159577689E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18193E+01
   Friction velocity        uet   :  0.99317E-02 0.85877E+00
   Friction velocity        uk    :  0.99317E-02 0.13976E+01
   Dimensionless distance   yplus :  0.24564E-01 0.33768E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.7044E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44047E-01      23   0.46488E-04   0.29694E+01 0.17222E+03 
c  Velocity[X]                                      0.24109E+01 
c  Velocity[Y]                                      0.55843E+00 
c  Velocity[Z]                                      0.38697E-09 
c  Pressure     0.32519E-09    1730   0.17964E-02   0.51651E+00 0.17285E+03 
c  Void Fractio 0.47857E-08      37   0.60774E-08   0.93942E-02 0.46034E+04 
c  k            0.29586E-03      23   0.17285E-06   0.54916E-03 0.45530E+03 
c  omega        0.41239E+18       2   0.57306E-16   0.24200E+21 0.19980E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.9728e-06                             8
a  omega             -6.5774e+06                             9
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4612          11.629          6.5835          4.2205
v  Velocity[Y]             -3.166          2.9643       -0.090302        -0.29289
v  Velocity[Z]         -0.0013954       0.0014769      3.9745e-08      7.5726e-10
v  ǁVelocityǁ           0.0048346          11.633          6.6632          4.2397
v  Pressure                  1921           59920           40511           54872
v  Void Fraction       3.0415e-18          0.9697       0.0081743      0.00018231
v  k                   1.8594e-16          1.4415        0.015431        0.021913
v  omega                    1e-24      6.6092e+10      2.9117e+06           97353
v  scalar1                      0               0               0               0
v  TurbVisc            1.4808e-22         0.24355        0.012941         0.12491
v  CourantNb            0.0004424          4.4012         0.83567         0.12052
v  FourierNb            0.0062244         0.82707         0.12156        0.067656
v  total_pressure            1921           59920           40511           54872
v  Density Old              30.98            1000          992.03          999.82


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016536          4.6695         0.95723         0.18817


 TIME FOR THE TIME STEP              108:        0.15278E+01

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


 INSTANT    0.545000000E-03   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159584763E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18182E+01
   Friction velocity        uet   :  0.65735E-01 0.84890E+00
   Friction velocity        uk    :  0.65734E-01 0.13964E+01
   Dimensionless distance   yplus :  0.16434E+00 0.33740E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.5456E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44050E-01      24   0.45134E-04   0.29779E+01 0.17246E+03 
c  Velocity[X]                                      0.24278E+01 
c  Velocity[Y]                                      0.55007E+00 
c  Velocity[Z]                                      0.30844E-09 
c  Pressure     0.64917E-09    1554   0.12751E-02   0.76059E+00 0.13971E+03 
c  Void Fractio 0.48364E-08      36   0.66019E-08   0.90206E-02 0.44688E+04 
c  k            0.29587E-03      23   0.93889E-07   0.49567E-03 0.43249E+03 
c  omega        0.20108E+09       4   0.56125E-07   0.60499E+20 0.19921E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -3.4308e-06                             8
a  omega             -9.1013e+06                            12
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4346          11.644          6.5802          4.2206
v  Velocity[Y]            -3.1649          2.9616       -0.090068        -0.29292
v  Velocity[Z]         -0.0014067       0.0014578      4.0381e-08      7.7468e-10
v  ǁVelocityǁ            0.009499          11.645          6.6605          4.2398
v  Pressure                1921.4           59830           40440           54844
v  Void Fraction       2.5198e-18         0.96961       0.0082716      0.00018503
v  k                   1.9961e-16          1.4654        0.015481        0.021915
v  omega                    1e-24      3.3048e+10      1.9814e+06           82867
v  scalar1                      0               0               0               0
v  TurbVisc            2.2327e-22         0.24356        0.012933         0.12488
v  CourantNb           0.00044038          4.3951         0.83534         0.12052
v  FourierNb            0.0062336         0.81143         0.12157        0.067577
v  total_pressure          1921.4           59830           40440           54844
v  Density Old             31.056            1000          991.93          999.82


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016543          4.6632         0.95692          0.1881


 TIME FOR THE TIME STEP              109:        0.14395E+01

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


 INSTANT    0.550000000E-03   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159591727E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18170E+01
   Friction velocity        uet   :  0.61566E-01 0.84187E+00
   Friction velocity        uk    :  0.61566E-01 0.13947E+01
   Dimensionless distance   yplus :  0.15391E+00 0.33699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.8301E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44053E-01      23   0.46558E-04   0.29683E+01 0.17217E+03 
c  Velocity[X]                                      0.24118E+01 
c  Velocity[Y]                                      0.55651E+00 
c  Velocity[Z]                                      0.27541E-09 
c  Pressure     0.19816E-09    1581   0.17127E-02   0.32882E+00 0.56590E+02 
c  Void Fractio 0.48885E-08      36   0.63579E-08   0.96025E-02 0.45679E+04 
c  k            0.29587E-03      23   0.63051E-07   0.45559E-03 0.41458E+03 
c  omega        0.48905E+08       5   0.11550E-06   0.15124E+20 0.19696E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.3432e-07                             7
a  omega             -2.3513e+05                            13
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4585          11.654          6.5768          4.2208
v  Velocity[Y]            -3.1858          2.9584       -0.089835        -0.29295
v  Velocity[Z]         -0.0014193       0.0014658      4.0487e-08      7.7754e-10
v  ǁVelocityǁ           0.0051736          11.655          6.6578            4.24
v  Pressure                1839.8           59815           40419           54836
v  Void Fraction       2.0876e-18         0.96978        0.008368      0.00018775
v  k                    2.141e-16          1.4636        0.015534        0.021916
v  omega                    1e-24      1.6526e+10      1.5157e+06           75608
v  scalar1                      0               0               0               0
v  TurbVisc            4.2684e-21         0.24356        0.012925         0.12486
v  CourantNb           0.00043827           4.394         0.83503         0.12053
v  FourierNb            0.0062431         0.80131         0.12159          0.0675
v  total_pressure          1839.8           59815           40419           54836
v  Density Old             31.266            1000          991.83          999.82


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016549          4.6608         0.95662         0.18803


 TIME FOR THE TIME STEP              110:        0.14614E+01

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


 INSTANT    0.555000000E-03   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159598678E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18158E+01
   Friction velocity        uet   :  0.13075E-01 0.83640E+00
   Friction velocity        uk    :  0.13074E-01 0.13942E+01
   Dimensionless distance   yplus :  0.32337E-01 0.33686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.7756E-13


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44056E-01      23   0.48182E-04   0.29917E+01 0.17284E+03 
c  Velocity[X]                                      0.24364E+01 
c  Velocity[Y]                                      0.55529E+00 
c  Velocity[Z]                                      0.35314E-09 
c  Pressure     0.17170E-08    1496   0.72677E-03   0.10017E+01 0.16306E+03 
c  Void Fractio 0.49409E-08      37   0.50827E-08   0.85216E-02 0.42637E+04 
c  k            0.29587E-03      22   0.62116E-07   0.58869E-03 0.47121E+03 
c  omega        0.42836E+14       2   0.82689E-13   0.37807E+19 0.18873E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.4635e-07                             8
a  omega             -1.1336e+07                            15
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.472          11.663          6.5735          4.2209
v  Velocity[Y]            -3.1871          2.9593       -0.089619        -0.29298
v  Velocity[Z]         -0.0014348        0.001481      4.1268e-08      7.9435e-10
v  ǁVelocityǁ           0.0067712          11.666          6.6551          4.2402
v  Pressure                1922.6           59928           40491           54868
v  Void Fraction       1.7294e-18         0.96984       0.0084631      0.00019049
v  k                   2.2946e-16          1.4564        0.015587        0.021918
v  omega                    1e-24      8.2655e+09      1.2831e+06           71978
v  scalar1                      0               0               0               0
v  TurbVisc            4.5784e-21         0.24356        0.012916         0.12483
v  CourantNb           0.00043629          4.3915         0.83475         0.12054
v  FourierNb            0.0062527         0.79688         0.12162        0.067423
v  total_pressure          1922.6           59928           40491           54868
v  Density Old             31.361            1000          991.74          999.82


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016556          4.6573         0.95637         0.18797


 TIME FOR THE TIME STEP              111:        0.13945E+01

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


 INSTANT    0.560000000E-03   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159605801E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18147E+01
   Friction velocity        uet   :  0.51941E-01 0.83200E+00
   Friction velocity        uk    :  0.51940E-01 0.13938E+01
   Dimensionless distance   yplus :  0.12985E+00 0.33676E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1265E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44060E-01      23   0.48374E-04   0.30778E+01 0.17530E+03 
c  Velocity[X]                                      0.25130E+01 
c  Velocity[Y]                                      0.56475E+00 
c  Velocity[Z]                                      0.18131E-09 
c  Pressure     0.38177E-09    1513   0.16636E-02   0.55080E+00 0.56863E+02 
c  Void Fractio 0.49943E-08      37   0.58227E-08   0.85112E-02 0.42226E+04 
c  k            0.29587E-03      22   0.54211E-07   0.55876E-03 0.45901E+03 
c  omega        0.59398E+11       2   0.34624E-10   0.94550E+18 0.16398E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -1.4201e-07                             8
a  omega             -4.4618e+05                            14
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4715          11.671          6.5702          4.2211
v  Velocity[Y]            -3.2102          2.9505       -0.089411        -0.29301
v  Velocity[Z]         -0.0014348       0.0014864      4.1222e-08      7.9415e-10
v  ǁVelocityǁ           0.0054573          11.674          6.6525          4.2404
v  Pressure                1923.5           59891           40491           54875
v  Void Fraction       1.4326e-18          0.9703       0.0085564      0.00019323
v  k                   2.4571e-16          1.4737        0.015641         0.02192
v  omega                    1e-24      4.1348e+09      1.1665e+06           70151
v  scalar1                      0               0               0               0
v  TurbVisc            4.9067e-21         0.24357        0.012908         0.12481
v  CourantNb           0.00043425          4.3622         0.83448         0.12055
v  FourierNb            0.0062623         0.82271         0.12164        0.067348
v  total_pressure          1923.5           59891           40491           54875
v  Density Old             31.186            1000          991.64          999.81


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016564          4.6282         0.95612          0.1879


 TIME FOR THE TIME STEP              112:        0.14190E+01

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


 INSTANT    0.565000000E-03   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159612999E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18137E+01
   Friction velocity        uet   :  0.46571E-01 0.11448E+01
   Friction velocity        uk    :  0.46571E-01 0.13924E+01
   Dimensionless distance   yplus :  0.11643E+00 0.33642E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1127
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.1789E-12


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44063E-01      22   0.47995E-04   0.30893E+01 0.17562E+03 
c  Velocity[X]                                      0.25082E+01 
c  Velocity[Y]                                      0.58114E+00 
c  Velocity[Z]                                      0.42008E-09 
c  Pressure     0.14231E-09    1725   0.18284E-02   0.23405E+00 0.10368E+03 
c  Void Fractio 0.50495E-08      37   0.65972E-08   0.86147E-02 0.42102E+04 
c  k            0.29587E-03      22   0.15817E-05   0.91636E-02 0.18588E+04 
c  omega        0.56668E+08       5   0.13224E-07   0.23876E+18 0.11694E+06 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction
a  k                 -2.8341e-07                             7
a  omega                  -50540                            15
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4962          11.676           6.567          4.2213
v  Velocity[Y]            -3.2108          2.9461       -0.089201        -0.29304
v  Velocity[Z]         -0.0014329       0.0014891      3.9956e-08      7.5804e-10
v  ǁVelocityǁ           0.0030953          11.677          6.6499          4.2406
v  Pressure                1294.8           59770           40446           54865
v  Void Fraction       1.1869e-18          0.9706       0.0086482      0.00019598
v  k                   2.6291e-16          1.4655        0.015687        0.021922
v  omega                    1e-24      2.0688e+09      1.1116e+06           69288
v  scalar1                      0               0               0               0
v  TurbVisc            5.2543e-21         0.24357        0.012901         0.12479
v  CourantNb           0.00043221          4.3441         0.83421         0.12056
v  FourierNb            0.0062718         0.84416         0.12167        0.067272
v  total_pressure          1294.8           59770           40446           54865
v  Density Old             31.126            1000          991.55          999.81


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016571          4.6098         0.95588         0.18783


 TIME FOR THE TIME STEP              113:        0.15112E+01

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


 INSTANT    0.570000000E-03   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159620207E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18132E+01
   Friction velocity        uet   :  0.34750E-01 0.10284E+01
   Friction velocity        uk    :  0.34750E-01 0.13895E+01
   Dimensionless distance   yplus :  0.86875E-01 0.33572E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1127
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100

@
@ @@ WARNING: Void fraction resolution
@    ========
@  The current time step is too large to ensure the min/max
@     principle on void fraction.
@
@  The current time step is  0.50000E-05 while
@     the maximum admissible value is  0.46113E-05
@
@  Clipping on void fraction should occur and
@     mass conservation is lost.
@ 


   ** CAVITATION MODELLING
      --------------------
   Mixture global mass budget: -0.7541E-10


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44066E-01      23   0.48246E-04   0.31295E+01 0.17674E+03 
c  Velocity[X]                                      0.25427E+01 
c  Velocity[Y]                                      0.58677E+00 
c  Velocity[Z]                                      0.61843E-09 
c  Pressure     0.11326E-07    1116   0.10560E-03   0.10100E+01 0.14943E+03 
c  Void Fractio 0.51076E-08      37   0.56748E-08   0.11963E-01 0.49170E+04 
c  k            0.29588E-03      23   0.16140E-05   0.11258E-01 0.20604E+04 
c  omega        0.42324E+09       3   0.10401E-08   0.59782E+17 0.67903E+05 
c  scalar1      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

   field             initial min     initial max  clips to min  clips to max
-  -------------  --------------  --------------  ------------  ------------
a  Void Fraction      9.8323e-19                         47442
a  k                 -4.8234e-07                             8
a  omega             -1.2649e+05                            15
a  scalar1      


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5554          11.681          6.5637          4.2215
v  Velocity[Y]            -3.2339          2.9449       -0.089016        -0.29307
v  Velocity[Z]         -0.0014299       0.0014894      4.0139e-08      7.6249e-10
v  ǁVelocityǁ             0.00322          11.681          6.6474          4.2408
v  Pressure                  1925           59847           40510           54898
v  Void Fraction            1e-10         0.97074       0.0087375      0.00019874
v  k                   2.8108e-16          1.4686        0.015727        0.021923
v  omega                    1e-24      1.0348e+09      1.0803e+06           68786
v  scalar1                      0               0               0               0
v  TurbVisc             5.622e-21         0.24357        0.012893         0.12476
v  CourantNb           0.00040762           4.353         0.83398         0.12057
v  FourierNb            0.0062812         0.84901         0.12169        0.067198
v  total_pressure            1925           59847           40510           54898
v  Density Old             30.669            1000          991.45          999.81


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016578           4.618         0.95568         0.18777


 TIME FOR THE TIME STEP              114:        0.11927E+01

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


 INSTANT    0.575000000E-03   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.159627606E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18126E+01
   Friction velocity        uet   :  0.26140E-01 0.11667E+01
   Friction velocity        uk    :  0.26140E-01 0.13864E+01
   Dimensionless distance   yplus :  0.63588E-01 0.33498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1128
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        100
SIGINT signal (Control+C or equivalent) received.
--> computation interrupted by user.

Call stack:
   1: 0x39d1809a23 <>                               (libgomp.so.1)
   2: 0x39d180859e <>                               (libgomp.so.1)
   3: 0x7ff4aa283e33 <cs_sles_it_solve+0x1853>        (libsaturne.so.0)
   4: 0x7ff4aa275dee <cs_multigrid_solve+0x87e>       (libsaturne.so.0)
   5: 0x7ff4aa2794bc <cs_sles_solve+0x2bc>            (libsaturne.so.0)
   6: 0x7ff4aa52ab59 <__cs_c_bindings_MOD_sles_solve_native+0x1ed> (libsaturne.so.0)
   7: 0x7ff4aa1285eb <resopv_+0x75db>                 (libsaturne.so.0)
   8: 0x7ff4aa10c9e9 <navstv_+0x42aa>                 (libsaturne.so.0)
   9: 0x7ff4aa139fb0 <tridim_+0x4800>                 (libsaturne.so.0)
  10: 0x7ff4aa0125d1 <caltri_+0x2b41>                 (libsaturne.so.0)
  11: 0x7ff4a9ff1d85 <cs_run+0x3e5>                   (libsaturne.so.0)
  12: 0x7ff4a9ff1f15 <main+0x135>                     (libsaturne.so.0)
  13: 0x39d001ed1d <__libc_start_main+0xfd>         (libc.so.6)
  14: 0x401609     <>                               (cs_solver)
End of stack

