command: 
 ./cs_solver --param Calc --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.2.1


  Copyright (C) 1998-2013 EDF S.A., France

  build Mi 15 Jan 2014 17:03:29 CET
  MPI version 2.2 (MPICH2 1.4.1)


  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:                Mi 15 Jan 2014 17:24:56 CET
  System:              Linux 3.8.0-35-generic
  Machine:             sebastian-GA-78LMT-USB3
  Processor:           model name	: AMD FX(tm)-4300 Quad-Core Processor
  Memory:              3431 MB
  User:                sebastian (sebastian)
  Directory:           /home/sebastian/opt/code_saturne-3.2.1/arch/Linux_x86_64/bin/RotFine/Case1/RESU/20140115-1724
  MPI ranks:           4 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    ParMETIS 4.0.3

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

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

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


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




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


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

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

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


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

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


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


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

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

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

  -- Continuous phase:

       RO0    =    0.10350E+04 (Reference density           )
       VISCL0 =    0.35000E-02 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             20 (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-epsilon           (ITURB = 20)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              1 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )


   - 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-epsilon           (ITURB = 20)
       Ce1    =    0.14400E+01 (Cepsilon 1: production coef.)
       CE2    =    0.19200E+01 (Cepsilon 2: dissipat.  coef.)
       SIGMAK =    0.10000E+01 (Prandtl relative to k       )
       SIGMAE =    0.13000E+01 (Prandtl relative to epsilon )
       CMU    =    0.90000E-01 (Cmu constant                )


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

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

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Pressure              0  0.1000E+01
 VelocityX             1  0.1000E+01
 VelocityY             1  0.1000E+01
 VelocityZ             1  0.1000E+01
 TurbEner              1  0.1000E+01
 Dissip                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
---------------------------------------------------------------------
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 VelocityX             1      1      1      1      0 0.10E+01 0.10E+01
 VelocityY             1      1      1      1      0 0.10E+01 0.10E+01
 VelocityZ             1      1      1      1      0 0.10E+01 0.10E+01
 TurbEner              1      1      1      1      0 0.00E+00 0.10E+01
 Dissip                1      1      1      1      0 0.00E+00 0.10E+01
-------------------------------------------------------------

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


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


 ** STOKES
    ------
       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
-------------------------------------------------------------------
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityX           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityY           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityZ           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 TurbEner            100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Dissip              100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Pressure              1     -1  0.1500E+01
 VelocityX             1     -1  0.1500E+01
 VelocityY             1     -1  0.1500E+01
 VelocityZ             1     -1  0.1500E+01
 TurbEner              1     -1  0.1500E+01
 Dissip                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                )


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


 ** CALCULATION OF TEMPORAL MEANS (MOMENTS)
    ---------------------------------------

       NBMOMT =              0 (Number of moments           )

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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Pressure              0  10000  0.1000E-07      1
 VelocityX            -1  10000  0.1000E-07      1
 VelocityY            -1  10000  0.1000E-07      1
 VelocityZ            -1  10000  0.1000E-07      1
 TurbEner             -1  10000  0.1000E-07      1
 Dissip               -1  10000  0.1000E-07      1
-----------------------------------

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


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


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

       NCEGRM =             30 (Max nb cells coarsest grid  )
       NGRMAX =             25 (Max number of levels        )
--------------------------------------
 Variable           IMGR NCYMAX NITMGF
--------------------------------------                       
 Pressure              1    100     10
 VelocityX             0    100     10
 VelocityY             0    100     10
 VelocityZ             0    100     10
 TurbEner              0    100     10
 Dissip                0    100     10
------------------------------

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


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

  Multigrid coarsening type: algebraic, face traveral by criteria

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


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

 --- Restarted calculation
       ISUITE =              0 (1: restarted calculation    )
       ILEAUX =              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 =             10 (Final time step required    )

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


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


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

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

 --- Post-processed variables

       Number Name
         2 Pressure        
         3 VelocityX       
         4 VelocityY       
         5 VelocityZ       
         6 TurbEner        
         7 Dissip          
        10 TurbVisc        
        11 CourantNb       
        12 FourierNb       
        13 total_pressure  
         --           --

 --- Probe history files
       NTHIST =             -1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              0 (Number of probes     )
       NTHSAV =             -1 (Checkpoint frequency )

       Number Name                  Nb. probes (-1: all)
         2 Pressure                      -1
         3 VelocityX                     -1
         4 VelocityY                     -1
         5 VelocityZ                     -1
         6 TurbEner                      -1
         7 Dissip                        -1
         8 Density                       -1
         9 LamVisc                       -1
        10 TurbVisc                      -1
        11 CourantNb                     -1
        12 FourierNb                     -1
        13 total_pressure                -1
        14 LocalTime                     -1
         --           --                --

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

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

         2 Pressure                       0
         3 VelocityX                      0
         4 VelocityY                      0
         5 VelocityZ                      0
         6 TurbEner                       0
         7 Dissip                         0
        10 TurbVisc                    -999
        11 CourantNb                   -999
        12 FourierNb                   -999
        13 total_pressure              -999
        14 LocalTime                   -999
         --           --                --

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


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


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

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


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


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: at calculation end


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

 Reading file:        mesh_input/mesh_02
 Finished reading:    mesh_input/mesh_02
 No "partition_input/domain_number_4" file available;

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

 Partitioning 1629817 cells to 4 domains on 4 ranks
   (ParMETIS_V3_PartKway).

  Total number of faces on parallel boundaries: 2976
  wall-clock time: 2.050927 s

  Number of cells per domain (histogramm):
    [     404591 ;     405573 [ =          3
    [     405573 ;     406555 [ =          0
    [     406555 ;     407537 [ =          0
    [     407537 ;     408519 [ =          0
    [     408519 ;     409502 [ =          0
    [     409502 ;     410484 [ =          0
    [     410484 ;     411466 [ =          0
    [     411466 ;     412448 [ =          0
    [     412448 ;     413430 [ =          0
    [     413430 ;     414413 ] =          1

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

 Partitioning finished (2.63 s)


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

 Halo construction with standard neighborhood
 ============================================

 Face interfaces creation
 Vertex interfaces creation
 Halo creation
 Halo definition
    Local halo definition
    Distant halo creation
    Updating the faces -> cells connectivity

 Histogram of the number of cells per rank:

    minimum value =             404591
    maximum value =             414413

      1 : [     404591 ;     406555 [ =          3
      2 : [     406555 ;     408519 [ =          0
      3 : [     408519 ;     410484 [ =          0
      4 : [     410484 ;     412448 [ =          0
      5 : [     412448 ;     414413 ] =          1

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

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

    minimum value =             405822
    maximum value =             415331

      1 : [     405822 ;     407723 [ =          3
      2 : [     407723 ;     409625 [ =          0
      3 : [     409625 ;     411527 [ =          0
      4 : [     411527 ;     413429 [ =          0
      5 : [     413429 ;     415331 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =                918
    maximum value =               2180

      1 : [        918 ;       1170 [ =          1
      2 : [       1170 ;       1422 [ =          2
      3 : [       1422 ;       1675 [ =          0
      4 : [       1675 ;       1927 [ =          0
      5 : [       1927 ;       2180 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =             782318
    maximum value =             801839

      1 : [     782318 ;     786222 [ =          1
      2 : [     786222 ;     790126 [ =          1
      3 : [     790126 ;     794030 [ =          0
      4 : [     794030 ;     797934 [ =          1
      5 : [     797934 ;     801839 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =              29456
    maximum value =              55021

      1 : [      29456 ;      34569 [ =          1
      2 : [      34569 ;      39682 [ =          0
      3 : [      39682 ;      44795 [ =          0
      4 : [      44795 ;      49908 [ =          1
      5 : [      49908 ;      55021 ] =          2

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        558
      2 : [          3 ;          4 ] =    1629259

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  1
    maximum value =                  3

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

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

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

 Writing file:        mesh_output
 Finished writing:    mesh_output

 Renumbering mesh:

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


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =             404735
    maximum value =             414505

      1 : [     404735 ;     406689 [ =          3
      2 : [     406689 ;     408643 [ =          0
      3 : [     408643 ;     410597 [ =          0
      4 : [     410597 ;     412551 [ =          0
      5 : [     412551 ;     414505 ] =          1

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               3312
    maximum value =               7491

      1 : [       3312 ;       4147 [ =          2
      2 : [       4147 ;       4983 [ =          0
      3 : [       4983 ;       5819 [ =          0
      4 : [       5819 ;       6655 [ =          0
      5 : [       6655 ;       7491 ] =          2

 Mesh coordinates:               minimum    and maximum
                       X : -2.9999624e+01  6.1540000e+01
                       Y : -3.3797720e+01  2.9999972e+01
                       Z :  0.0000000e+00  2.9000000e+01
 Mesh
     Number of cells:          1629817
     Number of interior faces: 3166344
     Number of boundary faces: 186580
     Number of vertices:       324245

 Groups:
    "Inlet"
       boundary faces:           46
    "Outlet"
       boundary faces:           58
    "boundary"
       boundary faces:        24811
    "cells"
       cells:                925211
    "wall"
       boundary faces:       161665

 --- Information on the volumes
       Minimum control volume      =  6.1486888e-09
       Maximum control volume      =  9.9096864e+00
       Total volume for the domain =  2.1709497e+04

  Criterion 1: Orthogonality:
    Number of bad cells detected: 3 -->   0 %

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 36600 -->   2 %

  Criterion 4: Cells Volume Ratio:
    Number of bad cells detected: 7 -->   0 %

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

 Warning:
 --------
    Mesh quality issue has been detected

    The mesh should be re-considered using the listed criteria.

    The calculation will run but the solution quality may be degraded...

 Computing geometric quantities (1.73 s)
  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 |  8.8095791330e-01   2.5257423202e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       111441
    Vertex-Vertex intersections:           13532
    Other intersections:                   97909

  Global number of new vertices to create:      61367

  Equivalences broken for 16 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 95578 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 333 faces (global).
  Join mesh cleaning done.

  Edge removed for 152 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0
                                                             
       ALMAX  =    0.27802E+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
 -----------------------------------------                   
  Pressure          0.0000E+00  0.0000E+00
  VelocityX         0.0000E+00  0.0000E+00
  VelocityY         0.0000E+00  0.0000E+00
  VelocityZ         0.0000E+00  0.0000E+00
  TurbEner          0.6000E-03  0.6000E-03
  Dissip            0.4758E-07  0.4758E-07
 ---------------------------------

  LocalTime         0.1000E-01  0.1000E-01
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1035E+04  0.1035E+04
  LamVisc           0.3500E-02  0.3500E-02
  TurbVisc          0.7048E+03  0.7048E+03
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          46
Smooth wall               5      161665
Rough wall                6           0
Symmetry                  4           0
Free outlet               3          58
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.61540E+02  -0.22826E+02   0.48947E+01



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46         0.000000000E+00
Smooth wall               5      161665         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.56582E+04
   Friction velocity        uet   :  0.00000E+00 0.44454E+03
   Friction velocity        uk    :  0.10953E-01 0.24064E+01
   Dimensionless distance   yplus :  0.54014E+01 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 |  1.1865866202e+01  -2.2314003068e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       106268
    Vertex-Vertex intersections:           10456
    Other intersections:                   95812

  Global number of new vertices to create:      60763

  Equivalences broken for 56 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 93028 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 435 faces (global).
  Join mesh cleaning done.

  Edge removed for 203 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      3.5085
 Global time                   (s):      3.8134

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.5613e-01; norm:  1.0018e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13926E+08    3584   0.65607E+01   0.90875E+00 
c  VelocityX    0.20081E+09     710   0.61005E-01   0.15903E+11 
c  VelocityY    0.20081E+09     710   0.61005E-01   0.17795E+10 
c  VelocityZ    0.20081E+09     710   0.61005E-01   0.43978E+09 
c  TurbEner     0.35564E+11     872   0.47332E-02   0.12274E+09 
c  Dissip       0.70426E+15    1381   0.47441E+01   0.10943E+22 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner 
a  Dissip   
a  LocalTime      6.2981e-06                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure            1.2396e+09      7.6566e+11      6.9984e+11      6.3248e+11
v  Velocity[x]        -1.4842e+05      2.4093e+05          5870.7          1486.5
v  Velocity[y]        -2.8452e+05           19410         -7752.1         -604.59
v  Velocity[z]        -1.1627e+05      1.2904e+05          1099.1          69.772
v  TurbEner            0.00059721          6010.2          186.64          143.78
v  Dissip              1.4695e-08      2.8229e+11      1.4142e+09      3.5919e+08
v  TurbVisc                704.84          704.84          704.84          704.84
v  CourantNb                    0               0               0               0
v  FourierNb            0.0015556          1587.8          13.475        0.056025
v  total_pressure      1.2397e+09      7.6566e+11      6.9984e+11      6.3248e+11


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0015556          1587.8          13.475        0.056021


 TIME FOR THE TIME STEP                1:        0.51593E+03

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


 INSTANT    0.119937019E-01   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.564473577E+09
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.564520201E+09
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31945E+08 0.60234E+05
   Friction velocity        uet   :  0.21255E-01 0.12185E+05
   Friction velocity        uk    :  0.13393E-01 0.42463E+02
   Dimensionless distance   yplus :  0.57364E+02 0.18968E+07
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145832
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 |  5.6862671987e+00  -2.4624781806e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       107257
    Vertex-Vertex intersections:           10513
    Other intersections:                   96744

  Global number of new vertices to create:      61515

  Equivalences broken for 41 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 94056 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 432 faces (global).
  Join mesh cleaning done.

  Edge removed for 195 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      6.5596
 Global time                   (s):      8.3902

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.5853e-01; norm:  1.0045e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.92952E+08    3584   0.32778E+01   0.16285E+01 
c  VelocityX    0.99433E+12     821   0.75374E+00   0.32021E+11 
c  VelocityY    0.99433E+12     821   0.75374E+00   0.53789E+10 
c  VelocityZ    0.99433E+12     821   0.75374E+00   0.13457E+10 
c  TurbEner     0.48659E+11     754   0.28561E-04   0.19478E+08 
c  Dissip       0.15305E+18     792   0.40256E-03   0.35875E+21 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner          -487.08                        211305
a  Dissip        -3.7769e+09                        227759
a  LocalTime      7.6976e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure            1.6509e+09      1.3979e+12      1.2826e+12      1.1485e+12
v  Velocity[x]        -3.5476e+05      5.5207e+05           14528          3559.4
v  Velocity[y]        -6.4011e+05           29769          -17592         -1505.1
v  Velocity[z]         -2.759e+05      2.9751e+05          2581.7          180.71
v  TurbEner            2.2854e-05          5118.2          140.19          100.59
v  Dissip              1.9494e-05      2.7834e+11      1.0831e+09      2.1318e+08
v  TurbVisc            5.5524e-10            2280         0.81659          23.327
v  CourantNb           0.00037211      1.2991e+05          1617.7          22.437
v  FourierNb           7.8241e-09         0.95418       0.0016534      0.00027023
v  total_pressure       1.651e+09      1.3979e+12      1.2826e+12      1.1485e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0010567      1.2991e+05          1617.7          22.435


 TIME FOR THE TIME STEP                2:        0.51333E+03

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


 INSTANT    0.139936942E-01   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.134526951E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.134536173E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12246E+09 0.83521E+05
   Friction velocity        uet   :  0.51012E-01 0.25308E+05
   Friction velocity        uk    :  0.59939E-02 0.39185E+02
   Dimensionless distance   yplus :  0.86080E+02 0.13926E+07
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141866
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -8.8084037560e-01  -2.5257427301e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       107331
    Vertex-Vertex intersections:           10427
    Other intersections:                   96904

  Global number of new vertices to create:      61352

  Equivalences broken for 29 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 94504 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 493 faces (global).
  Join mesh cleaning done.

  Edge removed for 229 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      3.0299
 Global time                   (s):      3.3349

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.5949e-01; norm:  1.0028e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.39227E+10    3584   0.14882E+01   0.18081E+02 
c  VelocityX    0.54633E+13     714   0.87631E+00   0.52396E+10 
c  VelocityY    0.54633E+13     714   0.87631E+00   0.62976E+10 
c  VelocityZ    0.54633E+13     714   0.87631E+00   0.89419E+10 
c  TurbEner     0.37161E+12     679   0.25362E-01   0.11534E+09 
c  Dissip       0.36475E+18     694   0.42731E-03   0.10694E+21 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner           -20088                        206955
a  Dissip        -7.6913e+09                        214394
a  LocalTime      3.3918e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -1.5118e+11       1.907e+12       1.782e+12      1.5583e+12
v  Velocity[x]           -4.3e+05      5.9194e+05           14747          3735.5
v  Velocity[y]        -6.7508e+05      1.8926e+05          -17032         -1806.1
v  Velocity[z]        -1.0685e+06      3.5249e+05          2318.4          190.88
v  TurbEner            0.00024422           88626          121.58          108.79
v  Dissip               0.0008801      2.7033e+11      9.3928e+08      1.1508e+08
v  TurbVisc             4.657e-16      5.4073e+05          2.7746          41.137
v  CourantNb           0.00094235      2.9483e+05          3688.8          27.699
v  FourierNb           8.7904e-09          448.43       0.0045013      0.00064857
v  total_pressure     -1.5118e+11       1.907e+12       1.782e+12      1.5583e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0036109      2.9483e+05          3688.8          27.696


 TIME FOR THE TIME STEP                3:        0.47361E+03

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


 INSTANT    0.159936908E-01   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.136384924E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.136388300E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48781E+08 0.31969E+06
   Friction velocity        uet   :  0.18257E+00 0.25948E+05
   Friction velocity        uk    :  0.94892E-02 0.16306E+03
   Dimensionless distance   yplus :  0.56751E+02 0.54601E+07
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135774
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -7.3879203108e+00  -2.4168825936e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       105613
    Vertex-Vertex intersections:            9825
    Other intersections:                   95788

  Global number of new vertices to create:      60821

  Equivalences broken for 46 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 93158 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 472 faces (global).
  Join mesh cleaning done.

  Edge removed for 218 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      2.3066
 Global time                   (s):      2.5854

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.5810e-01; norm:  1.0056e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.47232E+10    3059   0.30448E+00   0.21793E+01 
c  VelocityX    0.15893E+14     654   0.47101E+01   0.59341E+10 
c  VelocityY    0.15893E+14     654   0.47101E+01   0.75685E+10 
c  VelocityZ    0.15893E+14     654   0.47101E+01   0.11729E+11 
c  TurbEner     0.23037E+12     796   0.43157E-02   0.10474E+09 
c  Dissip       0.63258E+18     803   0.26620E-03   0.45093E+20 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner           -26726                        240200
a  Dissip        -7.9226e+09                        203170
a  LocalTime      3.6193e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -4.0861e+11      2.3978e+12      2.2575e+12      1.9617e+12
v  Velocity[x]           -4.8e+05      6.5552e+05           14884          3770.3
v  Velocity[y]        -7.3993e+05      1.7656e+05          -16855         -1797.2
v  Velocity[z]        -3.5031e+05      6.0773e+05          2316.6          199.01
v  TurbEner            1.7117e-05           96781          139.33          159.28
v  Dissip               0.0065305      2.6662e+11      8.5159e+08      7.4754e+07
v  TurbVisc            3.6402e-16      1.7963e+05          2.7812           53.97
v  CourantNb            0.0065827       2.763e+05          3596.1          26.632
v  FourierNb           1.1315e-08          113.68       0.0031823      0.00064761
v  total_pressure     -4.0861e+11      2.3978e+12      2.2575e+12      1.9617e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0082591       2.763e+05          3596.1          26.629


 TIME FOR THE TIME STEP                4:        0.43157E+03

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


 INSTANT    0.179936872E-01   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.135090384E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.135090613E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11363E+09 0.12267E+06
   Friction velocity        uet   :  0.86178E-01 0.29790E+05
   Friction velocity        uk    :  0.63361E-02 0.17039E+03
   Dimensionless distance   yplus :  0.45322E+02 0.52609E+07
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135963
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -1.3391527169e+01  -2.1433163875e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       106413
    Vertex-Vertex intersections:           11390
    Other intersections:                   95023

  Global number of new vertices to create:      60513

  Equivalences broken for 19 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 92415 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 404 faces (global).
  Join mesh cleaning done.

  Edge removed for 191 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0
 --- Information on the volumes
       Minimum control volume      = -9.4737646e-04
       Maximum control volume      =  9.9096864e+00
       Total volume for the domain =  2.1705071e+04

Abort due to the detection of a negative control volume.

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      2.3430
 Global time                   (s):      2.6412

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.6264e-01; norm:  1.0083e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.49826E+10    3584   0.38908E+00   0.12893E+01 
c  VelocityX    0.14558E+14     787   0.85396E+00   0.11989E+11 
c  VelocityY    0.14558E+14     787   0.85396E+00   0.12897E+11 
c  VelocityZ    0.14558E+14     787   0.85396E+00   0.17187E+11 
c  TurbEner     0.36497E+12     998   0.20474E-02   0.95337E+08 
c  Dissip       0.59452E+18    1039   0.13495E-03   0.17734E+20 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner           -34469                        276505
a  Dissip        -8.2338e+09                        166937
a  LocalTime      3.4832e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure            -5.796e+11      2.9515e+12      2.7519e+12      2.3938e+12
v  Velocity[x]        -5.3554e+05      6.8096e+05           14212          3810.3
v  Velocity[y]        -8.2203e+05      3.3541e+05          -16997         -1861.7
v  Velocity[z]          -7.77e+05      7.1848e+05          1940.9          201.17
v  TurbEner            4.6625e-05           92982          204.32          211.82
v  Dissip                0.026364      2.6197e+11      7.5416e+08       5.728e+07
v  TurbVisc            7.2693e-16      2.0412e+05          2.9875          93.012
v  CourantNb            0.0019659      2.8709e+05          3616.4          26.857
v  FourierNb            1.495e-08           145.4        0.003627      0.00075862
v  total_pressure      -5.796e+11      2.9515e+12      2.7519e+12      2.3938e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0035861      2.8709e+05          3616.4          26.856


 TIME FOR THE TIME STEP                5:        0.50132E+03

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


 INSTANT    0.199936837E-01   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.136920928E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.136922436E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46513E+08 0.31862E+06
   Friction velocity        uet   :  0.66664E-01 0.29792E+05
   Friction velocity        uk    :  0.73384E-02 0.16702E+03
   Dimensionless distance   yplus :  0.76734E+02 0.54158E+07
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     136149
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -1.8482526269e+01  -1.7236871420e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       103214
    Vertex-Vertex intersections:            9799
    Other intersections:                   93415

  Global number of new vertices to create:      60004

  Equivalences broken for 37 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 90612 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 1 set(s) of vertices.

  Edge removed for 458 faces (global).
  Join mesh cleaning done.

  Edge removed for 213 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      2.5672
 Global time                   (s):      2.8644

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.6387e-01; norm:  1.0050e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59399E+10    3584   0.51933E+00   0.12517E+01 
c  VelocityX    0.73263E+14     957   0.94562E+00   0.35032E+11 
c  VelocityY    0.73263E+14     957   0.94562E+00   0.26994E+11 
c  VelocityZ    0.73263E+14     957   0.94562E+00   0.29711E+11 
c  TurbEner     0.54754E+12    1034   0.28769E-02   0.33315E+09 
c  Dissip       0.52291E+18    1053   0.18662E-03   0.78972E+19 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner      -2.0128e+05                        296525
a  Dissip        -9.5486e+09                        200016
a  LocalTime      3.4944e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -6.8248e+11      3.5952e+12      3.2649e+12      2.8427e+12
v  Velocity[x]        -9.8635e+05      2.1156e+06           13335          3781.7
v  Velocity[y]        -8.3751e+05      1.2544e+06          -17120         -1974.6
v  Velocity[z]        -7.1533e+05        4.93e+05          1929.4          202.21
v  TurbEner            2.2313e-05      2.0128e+05          397.36           332.8
v  Dissip                0.016048      2.5795e+11       6.926e+08      4.4471e+07
v  TurbVisc            1.6634e-14      2.3524e+06          5.8923          210.38
v  CourantNb              -113.67      2.8617e+05          3582.3          28.796
v  FourierNb            -0.036612          920.96       0.0094465       0.0014993
v  total_pressure     -6.8248e+11      3.5952e+12      3.2649e+12      2.8427e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         -113.71      2.8617e+05          3582.3          28.794


 TIME FOR THE TIME STEP                6:        0.52776E+03

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


 INSTANT    0.219936802E-01   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.137349793E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.137353284E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32989E+08 0.46460E+06
   Friction velocity        uet   :  0.10538E+00 0.27577E+05
   Friction velocity        uk    :  0.74030E-02 0.16346E+03
   Dimensionless distance   yplus :  0.94105E+02 0.53140E+07
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133714
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on         58
  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -2.2313975458e+01  -1.1865918122e+01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       107902
    Vertex-Vertex intersections:           11189
    Other intersections:                   96713

  Global number of new vertices to create:      61411

  Equivalences broken for 41 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 93868 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 415 faces (global).
  Join mesh cleaning done.

  Edge removed for 193 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      3.6725
 Global time                   (s):      3.9848

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.6240e-01; norm:  9.9969e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.90653E+10    3584   0.45648E+00   0.13646E+01 
c  VelocityX    0.35162E+16     848   0.96197E+00   0.23370E+12 
c  VelocityY    0.35162E+16     848   0.96197E+00   0.11210E+12 
c  VelocityZ    0.35162E+16     848   0.96197E+00   0.94603E+11 
c  TurbEner     0.89872E+12    2148   0.47830E-02   0.32917E+10 
c  Dissip       0.37040E+18    1950   0.25212E-03   0.47244E+19 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner      -2.1439e+05                        318936
a  Dissip        -6.8081e+09                        200766
a  LocalTime      3.4602e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -7.6183e+11      4.5306e+12      3.7566e+12      3.2677e+12
v  Velocity[x]        -4.5073e+06      4.7672e+06           12948            3763
v  Velocity[y]        -2.1064e+06       2.859e+06          -17066           -2090
v  Velocity[z]        -1.2322e+06      1.3137e+06          1062.3          266.84
v  TurbEner            0.00019246      3.1695e+05          905.26             623
v  Dissip                 0.01398      2.5317e+11      6.4686e+08      3.8876e+07
v  TurbVisc            2.5087e-15      1.0968e+06          13.312          214.24
v  CourantNb             0.008681        2.89e+05          3474.9           31.96
v  FourierNb           1.4953e-08          386.39        0.017639       0.0023185
v  total_pressure     -7.6183e+11      4.5306e+12      3.7566e+12      3.2677e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010737        2.89e+05          3474.9          31.965


 TIME FOR THE TIME STEP                7:        0.62500E+03

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


 INSTANT    0.239936768E-01   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.137435504E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.137437487E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53545E+08 0.36106E+06
   Friction velocity        uet   :  0.42010E-01 0.26707E+05
   Friction velocity        uk    :  0.14833E-01 0.18837E+03
   Dimensionless distance   yplus :  0.48754E+02 0.68475E+07
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127292
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on         58
  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -2.4624768575e+01  -5.6863244955e+00   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       109432
    Vertex-Vertex intersections:           11825
    Other intersections:                   97607

  Global number of new vertices to create:      61802

  Equivalences broken for 20 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 95323 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 443 faces (global).
  Join mesh cleaning done.

  Edge removed for 201 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      5.7181
 Global time                   (s):      6.0536

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.6810e-01; norm:  1.0016e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.16807E+11    3122   0.48092E+00   0.17093E+01 
c  VelocityX    0.60867E+16    1556   0.89018E+00   0.10967E+13 
c  VelocityY    0.60867E+16    1556   0.89018E+00   0.47563E+12 
c  VelocityZ    0.60867E+16    1556   0.89018E+00   0.35007E+12 
c  TurbEner     0.33368E+13    2932   0.16779E-01   0.13080E+11 
c  Dissip       0.16142E+19    2518   0.77142E-03   0.77230E+21 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner      -6.6771e+05                        330707
a  Dissip         -1.363e+10                        218027
a  LocalTime       3.143e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -8.2485e+11      5.8364e+12      4.2222e+12      3.6737e+12
v  Velocity[x]        -1.0238e+07       1.463e+07           12032          3259.8
v  Velocity[y]        -5.0159e+06      8.6662e+06          -16954         -2466.6
v  Velocity[z]        -4.1972e+06      1.6747e+06          1466.1           232.6
v  TurbEner            0.00017793      6.6771e+05          1747.2            1195
v  Dissip                 0.20877       2.393e+11        6.98e+08      1.2986e+08
v  TurbVisc            1.4641e-13      5.4558e+06          79.421          975.28
v  CourantNb            0.0077416      3.1816e+05          3519.8          36.678
v  FourierNb          -3.8449e-05          7372.1           0.113        0.013004
v  total_pressure     -8.2485e+11      5.8364e+12      4.2222e+12      3.6737e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010401      3.1816e+05          3519.9          36.666


 TIME FOR THE TIME STEP                8:        0.73265E+03

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


 INSTANT    0.259936736E-01   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.136413274E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.136414465E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62358E+08 0.18778E+06
   Friction velocity        uet   :  0.27266E+00 0.31707E+05
   Friction velocity        uk    :  0.18199E-01 0.18098E+03
   Dimensionless distance   yplus :  0.77209E+02 0.13479E+08
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     108928
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         58
  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -2.5257429350e+01   8.8078160674e-01   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       105263
    Vertex-Vertex intersections:            9702
    Other intersections:                   95561

  Global number of new vertices to create:      60665

  Equivalences broken for 37 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 92877 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 405 faces (global).
  Join mesh cleaning done.

  Edge removed for 187 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      2.6289
 Global time                   (s):      2.9563

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.5361e-01; norm:  1.0025e-11

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.32441E+11    2816   0.21971E+00   0.12684E+01 
c  VelocityX    0.93024E+17    2236   0.91642E+00   0.49148E+13 
c  VelocityY    0.93024E+17    2236   0.91642E+00   0.29386E+13 
c  VelocityZ    0.93024E+17    2236   0.91642E+00   0.15869E+13 
c  TurbEner     0.41115E+14    5544   0.15949E+01   0.18896E+12 
c  Dissip       0.76821E+19    6344   0.40024E+00   0.12638E+23 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner      -3.1632e+05                        295464
a  Dissip        -7.4142e+09                        158216
a  LocalTime      2.9133e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -8.4317e+11      7.6166e+12      4.5726e+12      3.9671e+12
v  Velocity[x]        -4.0821e+07      1.4262e+07           11946          3430.5
v  Velocity[y]        -3.0477e+07      8.4483e+06          -17235         -2823.8
v  Velocity[z]        -7.4264e+06      9.9299e+06         -337.23          512.67
v  TurbEner            0.00013594      6.3595e+06            3279          1888.2
v  Dissip                 0.85395      3.8884e+11      1.6742e+09      1.1759e+09
v  TurbVisc              4.52e-14      3.5741e+08          405.52          638.05
v  CourantNb            0.0063443      3.4325e+05          3507.7          53.192
v  FourierNb           1.5756e-08           55611         0.31605        0.054581
v  total_pressure     -8.4317e+11      7.6166e+12      4.5726e+12      3.9671e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0078795      3.4325e+05          3508.1          53.268


 TIME FOR THE TIME STEP                9:        0.11080E+04

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


 INSTANT    0.279936707E-01   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.128678533E+10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          58         0.128681843E+10
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16909E+09 0.28846E+05
   Friction velocity        uet   :  0.17812E+00 0.40324E+05
   Friction velocity        uk    :  0.14583E-01 0.26655E+03
   Dimensionless distance   yplus :  0.67190E+02 0.12952E+08
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134304
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     161665
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on         58
  Global number of boundary faces selected for joining:      24811
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      10736 |    0.039379 | -2.4168843126e+01   7.3878640748e+00   8.5000000000e+00 | ORI
     193377 |    0.465602 |  2.0738658579e+01   1.8812443763e+01   5.8167990191e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       105487
    Vertex-Vertex intersections:            9550
    Other intersections:                   95937

  Global number of new vertices to create:      60492

  Equivalences broken for 64 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 93325 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 424 faces (global).
  Join mesh cleaning done.

  Edge removed for 200 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

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

   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      3.2111
 Global time                   (s):      3.5786

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.6414e-01; norm:  9.9743e-12


 Write final restart files
   checkpoint at iteration         10, Physical time    0.28994E-01


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

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 End writing

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

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
 End writing


 Time for restart files:    0.77085E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.48746E+11    3571   0.50460E+00   0.17890E+01 
c  VelocityX    0.11401E+18    3961   0.59489E+00   0.99665E+13 
c  VelocityY    0.11401E+18    3961   0.59489E+00   0.58813E+13 
c  VelocityZ    0.11401E+18    3961   0.59489E+00   0.65337E+13 
c  TurbEner     0.96567E+14    7350   0.10713E-02   0.18686E+11 
c  Dissip       0.77821E+20    7811   0.36816E-04   0.21866E+22 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  TurbEner      -2.4121e+06                        317668
a  Dissip        -5.5574e+09                        249661
a  LocalTime      2.2459e-09                        414413


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -7.4173e+11      1.0396e+13      5.0675e+12      4.3983e+12
v  Velocity[x]         -2.254e+07      1.2491e+07           10495          3093.8
v  Velocity[y]        -1.4731e+07      6.6073e+06          -15647         -2940.6
v  Velocity[z]        -6.7872e+06      5.5379e+06          2554.8         -141.37
v  TurbEner            0.00013013       6.201e+06          3945.2          2178.5
v  Dissip                  1.1697      3.7946e+11      1.4247e+09      9.4113e+08
v  TurbVisc            8.2032e-14      9.0864e+06          57.678          673.65
v  CourantNb           0.00055851      4.4525e+05          3433.4          64.711
v  FourierNb            1.252e-08          5282.8        0.057283        0.008657
v  total_pressure     -7.4173e+11      1.0396e+13      5.0675e+12      4.3983e+12


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0026048      4.4525e+05          3433.5          64.673


 TIME FOR THE TIME STEP               10:        0.15241E+04

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.77661E-01
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:           6799.032 s
  System CPU time:           18.656 s
  Total CPU time:         27294.852 s

  Elapsed time:            6968.294 s
  CPU / elapsed time          0.978

Memory use summary:

  Total memory used:                               3.044 GiB
                             local minimum:      759.590 MiB  (rank 3)
                             local maximum:      792.008 MiB  (rank 2)
  Theoretical instrumented dynamic memory:         1.418 GiB
                             local minimum:      353.114 MiB  (rank 3)
                             local maximum:      372.838 MiB  (rank 2)
