command: 
 ./cs_solver --mpi

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

                                  (R)
                      Code_Saturne

                      Version 4.2.0


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

  revision 4.2.0
  build Thu Feb  4 07:35:38 2016
  MPI version 3.0 (Open MPI 1.8.0)


  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:                Mon Mar 21 09:19:55 2016
  System:              Linux 2.6.32-431.el6.x86_64
  Machine:             nxb3a19
  Processor:           model name	: Intel(R) Xeon(R) CPU E5-2697 v2 @ 2.70GHz
  Memory:              64530 MB
  User:                vxm64-rja16 (vxm64-rja16)
  Directory:           /gpfs/stfc/local/HCP086/rja16/vxm64-rja16/CTM1/GinW60_100Hz/RESU/20160321-0919
  MPI ranks:           120 (appnum attribute: 0)
  OpenMP threads:      1
  Processors/node:     1
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

 Reading metadata from file: "mesh_input"

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

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


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




Warning: computation of time moment "Velocity_mean"will be reset,
           as restart data for "Velocity_mean" is not available.

Warning: computation of time moment "Velocity_variance"will be reset,
           as restart data for "Velocity_variance" is not available.

Warning: computation of time moment "uu_mean"will be reset,
           as restart data for "uu_mean" is not available.

Warning: computation of time moment "vv_mean"will be reset,
           as restart data for "vv_mean" is not available.

Warning: computation of time moment "ww_mean"will be reset,
           as restart data for "ww_mean" is not available.

Warning: computation of time moment "uv_mean"will be reset,
           as restart data for "uv_mean" is not available.

Warning: computation of time moment "uw_mean"will be reset,
           as restart data for "uw_mean" is not available.

Warning: computation of time moment "vw_mean"will be reset,
           as restart data for "vw_mean" is not available.

Warning: computation of time moment "Wr_moy"will be reset,
           as restart data for "Wr_moy" is not available.

Warning: computation of time moment "Wt_moy"will be reset,
           as restart data for "Wt_moy" is not available.

Warning: computation of time moment "Wa_moy"will be reset,
           as restart data for "Wa_moy" is not available.

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


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

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

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


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

 --- Physics
       NVAR   =              8 (Nb variables                )
       NSCAL  =              2 (Nb scalars                  )
       NSCAUS =              2 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.11576E+04 (Reference density           )
       VISCL0 =    0.10660E-01 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

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


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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             20 (Turbulence model            )
       IWALLF =              2 (wall function               )
                               (0: disabled                 )
                               (1: one scale power law
                                   (forbidden for k-epsilon))
                               (2: one scale log law        )
                               (3: two scales log law       )
                               (4: scalable wall function   )
                               (5: two scales V. Driest     )
                               (6: two scales smooth/rough  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - k-epsilon           (ITURB = 20)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.20000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              1 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )


   - Rotation/curvature correction
       IRCCOR =              1 (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                )

   - Rotation/curvature correction (Cazalbou)
       CCAZE2 =    0.18300E+01 (Coef Ce2^0                  )
       CCAZSC =    0.11900E+00 (Coef Csc                    )
       CCAZA  =    0.43000E+01 (Coef a                      )
       CCAZB  =    0.51300E+01 (Coef b                      )
       CCAZC  =    0.45300E+00 (Coef c                      )
       CCAZD  =    0.68200E+00 (Coef d                      )


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.20000E-06 (Minimum time step           )
       DTMAX  =    0.20000E-02 (Maximum time step           )
       DTREF  =    0.20000E-05 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
 Turb Kinetic Ene      1  0.1000E+01
 Turb Dissipation      1  0.1000E+01
 Tracer                1  0.1000E+01
 Variance_Tracer       1  0.1000E+01
----------------------------

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

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

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


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

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Velocity              1      1      1      1      0 0.00E+00 0.10E+01
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 Turb Kinetic Ene      1      1      1      1      0 0.00E+00 0.10E+01
 Turb Dissipation      1      1      1      1      0 0.00E+00 0.10E+01
 Tracer                1      1      1      1      0 0.00E+00 0.10E+01
 Variance_Tracer       1      1      1      1      0 0.00E+00 0.10E+01
-------------------------------------------------------------

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

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

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


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


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

       IMRGRA =              3 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 Pressure            100      5  0.1000E-04  0.1000E-06  0.0000E+00
 Turb Kinetic Ene    100      2  0.1000E-04  0.1000E-06  0.0000E+00
 Turb Dissipation    100      2  0.1000E-04  0.1000E-06  0.0000E+00
 Tracer              100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Variance_Tracer     100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              1      1  0.1500E+01
 Pressure              1      1  0.1500E+01
 Turb Kinetic Ene      0      1  0.1500E+01
 Turb Dissipation      0      1  0.1500E+01
 Tracer                1      1  0.1500E+01
 Variance_Tracer       1      1  0.1500E+01
-----------------------------------

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


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


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


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
 Turb Kinetic Ene  0.1000E-07      1
 Turb Dissipation  0.1000E-07      1
 Tracer            0.1000E-07      1
 Variance_Tracer   0.1000E-07      1
------------------------------------

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


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


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

-------------------------------------------------------------
 Variable         Number ISCACP  ITURT     VISLS0      SIGMAS
-------------------------------------------------------------
 Tracer                1      0      0  0.1066E-01  0.1000E+01
 Variance_Tracer       2      0      0  0.1066E-01  0.1000E+01
---------------------------------------------------------------------

------------------------------------
 Variable         Number      RVARFL
------------------------------------
 Tracer                1  0.8000E+00
 Variance_Tracer       2  0.8000E+00
-------------------------------------------

-------------------------------------------------------
 Variable         Number ICLVFL      SCAMIN      SCAMAX
-------------------------------------------------------
 Tracer                1     -1  0.0000E+00  0.1000E+01
 Variance_Tracer       2      0 -0.1000E+13  0.1000E+13
-------------------------------------------------------

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

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

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

------------------------------------------------------
   Scalar        THETSS    IVSEXT      THETVS
------------------------------------------------------
          1  0.0000E+00         0  0.0000E+00
          2  0.0000E+00         0  0.0000E+00
------------------------------------------------------

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


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


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

 --- Restarted calculation
       ISUITE =              1 (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 =         120000 (Final time step required    )

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


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


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

 --- Restart file
       NTSUIT =           1000 (Checkpoint frequency )

 --- Post-processed variables


Velocity
Pressure
Turb Kinetic Energy
Turb Dissipation
Tracer
Variance_Tracer
Laminar Viscosity
Turb Viscosity
CFL
Fourier Number
Total Pressure
Yplus
u_mean
v_mean
w_mean
Velocity_mean
Velocity_variance
uu_mean
vv_mean
ww_mean
uv_mean
uw_mean
vw_mean
Wr_moy
Wt_moy
Wa_moy
p_mean
k_mean
k_var
eps_mean
eps_var
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =             16 (Number of probes     )
       NTHSAV =              1 (Checkpoint frequency )

       Number Name                  Nb. probes (-1: all)
         2 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 Turb Kinetic Ene              -1
         7 Turb Dissipation              -1
         8 Tracer                        -1
         9 Variance_Tracer               -1
        12 Turb Viscosity                -1
        16 u_mean                        -1
        17 v_mean                        -1
        18 w_mean                        -1
        19 Velocity_mean                 -1
        20 Velocity_varianc              -1
        21 uu_mean                       -1
        22 vv_mean                       -1
        23 ww_mean                       -1
        24 uv_mean                       -1
        25 uw_mean                       -1
        26 vw_mean                       -1
        27 Wr_moy                        -1
        28 Wt_moy                        -1
        29 Wa_moy                        -1
        30 p_mean                        -1
        31 k_mean                        -1
        32 k_var                         -1
        33 eps_mean                      -1
        34 eps_var                       -1
         --           --                --

 --- Log files
       NTLIST =             10 (Output frequency     )

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

         2 Velocity                       0
         5 Pressure                       0
         6 Turb Kinetic Ene               0
         7 Turb Dissipation               0
         8 Tracer                         0
         9 Variance_Tracer                0
        11 Laminar Viscosit            -999
        12 Turb Viscosity              -999
        13 CFL                         -999
        14 Fourier Number              -999
        15 Total Pressure              -999
        16 u_mean                      -999
        17 v_mean                      -999
        18 w_mean                      -999
        19 Velocity_mean               -999
        20 Velocity_varianc            -999
        21 uu_mean                     -999
        22 vv_mean                     -999
        23 ww_mean                     -999
        24 uv_mean                     -999
        25 uw_mean                     -999
        26 vw_mean                     -999
        27 Wr_moy                      -999
        28 Wt_moy                      -999
        29 Wa_moy                      -999
        30 p_mean                      -999
        31 k_mean                      -999
        32 k_var                       -999
        33 eps_mean                    -999
        34 eps_var                     -999
         --           --                --

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


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


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

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


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


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: 
      time dependency: transient connectivity
      output: every 400 time steps and at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input
 No "partition_input/domain_number_120" file available;

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

 Partitioning by space-filling curve: Hilbert (in bounding box).
  Number of cells per domain (histogramm):
    [      23267 ;      23268 ] =        120

 Partitioning finished (25.6 s)


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

 Halo construction with extended neighborhood
 ============================================

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

 Histogram of the number of cells per rank:

    minimum value =              23267
    maximum value =              23268

      1 : [      23267 ;      23268 ] =        120

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

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

    minimum value =              28841
    maximum value =              36637

      1 : [      28841 ;      30400 [ =         20
      2 : [      30400 ;      31959 [ =         31
      3 : [      31959 ;      33518 [ =         44
      4 : [      33518 ;      35077 [ =         22
      5 : [      35077 ;      36637 ] =          3

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

 Histogram of the number of ghost cells per rank:

    minimum value =               5574
    maximum value =              13370

      1 : [       5574 ;       7133 [ =         20
      2 : [       7133 ;       8692 [ =         31
      3 : [       8692 ;      10251 [ =         44
      4 : [      10251 ;      11810 [ =         22
      5 : [      11810 ;      13370 ] =          3

 Histogram of the number of ghost cells
 in the standard neighborhood per rank:

    minimum value =               3090
    maximum value =               6013

      1 : [       3090 ;       3674 [ =         22
      2 : [       3674 ;       4259 [ =         27
      3 : [       4259 ;       4843 [ =         35
      4 : [       4843 ;       5428 [ =         29
      5 : [       5428 ;       6013 ] =          7

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

 Histogram of the number of interior faces per rank:

    minimum value =              52992
    maximum value =              65437

      1 : [      52992 ;      55481 [ =          9
      2 : [      55481 ;      57970 [ =         17
      3 : [      57970 ;      60459 [ =         39
      4 : [      60459 ;      62948 [ =         36
      5 : [      62948 ;      65437 ] =         19

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

 Histogram of the number of boundary faces per rank:

    minimum value =               2753
    maximum value =               7892

      1 : [       2753 ;       3780 [ =         38
      2 : [       3780 ;       4808 [ =         41
      3 : [       4808 ;       5836 [ =         17
      4 : [       5836 ;       6864 [ =         14
      5 : [       6864 ;       7892 ] =         10

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                 15

      1 : [          3 ;          5 [ =    1806630
      2 : [          5 ;          7 [ =     842208
      3 : [          7 ;         10 [ =     109721
      4 : [         10 ;         12 [ =      33317
      5 : [         12 ;         15 ] =        176

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  6
    maximum value =                 31

      1 : [          6 ;         11 [ =         57
      2 : [         11 ;         16 [ =         60
      3 : [         16 ;         21 [ =          1
      4 : [         21 ;         26 [ =          1
      5 : [         26 ;         31 ] =          1

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

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

 Renumbering mesh:

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

   renumbering for interior faces:
     cell adjacency pre-ordering:         lowest id first
     faces adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for boundary faces:
     numbering:                           none

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

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =              23267
    maximum value =              35197

      1 : [      23267 ;      25653 [ =          2
      2 : [      25653 ;      28039 [ =         10
      3 : [      28039 ;      30425 [ =         53
      4 : [      30425 ;      32811 [ =         45
      5 : [      32811 ;      35197 ] =         10

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               2788
    maximum value =              11148

      1 : [       2788 ;       4460 [ =         21
      2 : [       4460 ;       6132 [ =         48
      3 : [       6132 ;       7804 [ =         35
      4 : [       7804 ;       9476 [ =         10
      5 : [       9476 ;      11148 ] =          6

 Mesh coordinates:               minimum    and maximum
                       X : -4.2646695e-02  4.2649990e-02
                       Y :  2.5000000e-02  9.0000000e-02
                       Z : -4.2649594e-02  4.2647132e-02
 Mesh
     Number of cells:          2792052
     Number of interior faces: 6911262
     Number of boundary faces: 551430
     Number of vertices:       1992548

 Groups:
    "ar"
       cells:                600000
    "ar_wall"
       interior faces:       254051
       boundary faces:        57724
    "as"
       cells:                600000
    "as_wall"
       interior faces:       295675
       boundary faces:        47460
    "cr"
       cells:                759087
    "cr_circ"
       interior faces:       254051
    "cr_wall"
       boundary faces:        91958
    "crv1"
       cells:                 58304
    "crv2"
       cells:                 64768
    "crv3"
       cells:                 58335
    "crv4"
       cells:                 68997
    "crv5"
       cells:                 63942
    "crv6"
       cells:                 64129
    "cs"
       cells:                832965
    "cs_circ"
       interior faces:       295675
    "cs_i1"
       boundary faces:           21
    "cs_i2"
       boundary faces:           11
    "cs_i3"
       boundary faces:           19
    "cs_wall"
       boundary faces:        98237
    "inletr"
       boundary faces:         4000
    "inlets"
       boundary faces:         4000
    "outlet"
       boundary faces:         8000
    "rotor_interface"
       boundary faces:       120000
    "stator_interface"
       boundary faces:       120000

 --- Information on the volumes
       Minimum control volume      =  1.5125463e-12
       Maximum control volume      =  1.2760931e-09
       Total volume for the domain =  9.1233461e-05

  Criterion 1: Orthogonality:
    Number of bad cells detected: 4019 -->   0 %

  Criterion 2: Offset:
    Number of bad cells detected: 177807 -->   6 %

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 1620 -->   0 %

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

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

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

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

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

 Computing geometric quantities (0.213 s)

 Extended neighborhood reduced by non-orthogonality
 --------------------------------------------------

 Size of complete cell-cell connectivity:    121910910
 Size of filtered cell-cell conectivity:       6722901
 115188009 connections removed, for a ratio of  5.5 % used
                                                             
       ALMAX  =    0.45018E-01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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

   ** READING MAIN AND AUXILIARY RESTART FILES
      ----------------------------------------


      READING THE MAIN RESTART FILE

 Start reading

  Warning: the number of variables or properties has been changed
           relative to the restart file.

  current:  4 model and 2 user variables
            11 model and 0 user properties
  previous: 4 model and 1 user variables
            11 model and 0 user properties

  The computation continues, with a partial restart.
 Reading dimensions complete
  Reading the previous time step number (restarting computation)  NTPABS =       110000
  Reading the previous time step number (restarting computation)  TTPABS =   0.1600E+00
  Reading the previous moving mesh moment (restarting computation)  TTPMOB =   0.1600E+00
 Reading options complete
  restart/main: section "Variance_Tracer::vals::0" not present.

  Warning: the following variables could not be found or read
           in restart file "restart/main", so default initializations
           will be used:

  Variance_Tracer

  Read variables from restart: restart/main
 Reading complete

         READING THE AUXILIARY RESTART FILE             

 Start reading                                          
   Fin de la lecture des options                        
   Fin de la lecture des proprietes physiques           
   Fin de la lecture du pas de temps                    
   Fin de la lecture des flux de masse                  
  restart/auxiliary: section "Variance_Tracer::bc_coeffs::a" not present.
  restart/auxiliary: section "Variance_Tracer::bc_coeffs::b" not present.
  restart/auxiliary: section "Variance_Tracer::bc_coeffs::af" not present.
  restart/auxiliary: section "Variance_Tracer::bc_coeffs::bf" not present.


Code_Saturne: /gpfs/stfc/local/package_build/build/ccm87-build/BLUEWONDER2/SATURNE/SATURNE_4.2.0-gcc_4.9.1_OPENMPI_1.8/saturne-4.2.0-gcc_4.9.1_OPENMPI_1.8/src/base/cs_restart_default.c:2309: Warning

Some boundary condition coefficients could not be read from a restart file;
they will be initialized with default values.

   Fin de la lecture des conditions aux limites         
   Fin de la lecture des termes sources                 
 End reading                                            

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


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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity         -0.2826E+02  0.2864E+02
  Velocity         -0.1818E+02  0.1904E+02
  Velocity         -0.2801E+02  0.2850E+02
  Pressure         -0.5420E+06  0.8111E+06
  Turb Kinetic Ene  0.8815E-08  0.3318E+02
  Turb Dissipation  0.1546E-04  0.2865E+07
  Tracer            0.1139E-14  0.1000E+01
  Variance_Tracer   0.0000E+00  0.0000E+00
 ---------------------------------

                dt  0.2000E-05  0.2000E-05
 ---------------------------------


  ** Temporal moment accumulated weights
     -----------------------------------

   id   n it.             value
   ---- -------- --------------
   0    109974             0.16


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

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



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



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


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




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


 INSTANT    0.160002000E+00   TIME STEP NUMBER          110001
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1158E+04  0.1158E+04
  molecular_viscos  0.1066E-01  0.1066E-01
  turbulent_viscos  0.2100E-16  0.1901E+01
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 Tracer                1  0.1066E-01  0.1066E-01
 Variance_Tracer       2  0.1066E-01  0.1066E-01
 -----------------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2        8021
Smooth wall               5      295409
Rough wall                6           0
Symmetry                  4           0
Free outlet               3        8000
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with pressure Dirichlet condition detected
Update of reference point for total pressure
 XYZP0 =    0.14957E-01   0.90000E-01  -0.28862E-01



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        8021        -0.588521606E-01
Smooth wall               5      295409        -0.122987860E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        8000         0.181847615E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42852E+02 0.14522E+02
   Friction velocity        uet   :  0.42319E-01 0.37340E+01
   Friction velocity        uk    :  0.42319E-01 0.37340E+01
   Dimensionless distance   yplus :  0.90200E-01 0.45151E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      48162
   Nb of faces within the viscous sub-layer     :     104393
   Total number of wall faces                   :     295409
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step     110001
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160004000E+00   TIME STEP NUMBER          110002
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        8021        -0.643116256E-01
Smooth wall               5      295409        -0.132043364E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        8000         0.196362592E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42876E+02 0.14527E+02
   Friction velocity        uet   :  0.42521E-01 0.37284E+01
   Friction velocity        uk    :  0.42521E-01 0.37284E+01
   Dimensionless distance   yplus :  0.10067E+00 0.45112E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      48138
   Nb of faces within the viscous sub-layer     :     104391
   Total number of wall faces                   :     295409
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step     110002
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160006000E+00   TIME STEP NUMBER          110003
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160008000E+00   TIME STEP NUMBER          110004
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160010000E+00   TIME STEP NUMBER          110005
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160012000E+00   TIME STEP NUMBER          110006
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160014000E+00   TIME STEP NUMBER          110007
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160016000E+00   TIME STEP NUMBER          110008
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160018000E+00   TIME STEP NUMBER          110009
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160020000E+00   TIME STEP NUMBER          110010
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        8021        -0.643116256E-01
Smooth wall               5      295409        -0.132052057E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        8000         0.196371274E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40479E+02 0.14482E+02
   Friction velocity        uet   :  0.38862E-01 0.37347E+01
   Friction velocity        uk    :  0.38862E-01 0.37347E+01
   Dimensionless distance   yplus :  0.93872E-01 0.44926E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      48081
   Nb of faces within the viscous sub-layer     :     104404
   Total number of wall faces                   :     295409
------------------------------------------------------------



   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      0.6663
 Global time                   (s):      0.6864

Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63269E+03     158   0.20679E-05   0.43038E+03 0.11220E+04 
c  Velocity[X]                                      0.15795E+03 
c  Velocity[Y]                                      0.11071E+03 
c  Velocity[Z]                                      0.16172E+03 
c  Pressure     0.16407E-01     125   0.43945E-03   0.17972E+00 0.10986E+05 
c  Turb Kinetic 0.14921E+03     133   0.94002E-08   0.96033E+02 0.21856E+04 
c  Turb Dissipa 0.23400E+06     113   0.92159E-08   0.17721E+11 0.63841E+04 
c  Tracer       0.43154E+01      51   0.50308E-06   0.15699E-02 0.51922E+03 
c  Variance_Tra 0.45263E-01      50   0.84171E-05   0.81767E-02 0.37504E+05 
-----------------------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy        -0.22315                          6209
a  Turb Dissipation             -15698                             5
a  Tracer                                            1                           5
a  Variance_Tracer         -2.1811e-09                            77


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -28.296          28.657        -0.14246       -0.014396
v  Velocity[Y]                  -18.18          19.047          0.5743        0.072027
v  Velocity[Z]                     -28          28.526       -0.033262      0.00048616
v  ǁVelocityǁ                 0.012246          30.962          11.211          10.918
v  Pressure                -5.6176e+05      8.3346e+05      2.4131e+05      2.3416e+05
v  Turb Kinetic Energy      1.2405e-08          38.023           2.812           2.101
v  Turb Dissipation         1.6416e-05       3.051e+06           29777            4165
v  Tracer                   1.1331e-15               1        0.027006        0.031818
v  Variance_Tracer                   0          0.8529      1.0311e-05      6.5011e-06
v  Laminar Viscosity           0.01066         0.01066         0.01066         0.01066
v  Turb Viscosity           1.5439e-17          1.9104         0.13753         0.20427
v  CFL                      0.00033946          2.0283         0.11155        0.056496
v  Fourier Number           0.00025665          25.583         0.59641        0.051455
v  Total Pressure          -4.6043e+05      9.3479e+05      3.4263e+05      3.3548e+05
m  u_mean                       -14.55          14.794       -0.015208      -0.0079032
m  v_mean                      -17.338          9.7253         0.67625        0.059737
m  w_mean                      -14.916          15.174      -0.0076509     -0.00011109
m  Velocity_mean              0.010303          30.968          11.206          10.914
m  Velocity_variance        4.5576e-11           10.07       0.0083608       0.0017115
m  uu_mean                  2.5394e-08          821.02          76.503          80.033
m  vv_mean                  6.6349e-08          363.59          11.851          11.623
m  ww_mean                  3.4646e-08          811.76          76.308          79.158
m  uv_mean                     -414.63          341.84        -0.02651        0.093841
m  uw_mean                     -403.84          378.47          -0.846       -0.038034
m  vw_mean                     -353.11          270.52        0.046483        -0.13583
m  Wr_moy                          inf            -inf            -nan            -nan
m  Wt_moy                          inf            -inf            -nan            -nan
m  Wa_moy                            0               0               0               0
m  p_mean                  -6.5298e+05      9.8898e+05      2.3713e+05      2.2964e+05
m  k_mean                   9.1199e-06          13.435          3.2716           2.487
m  k_var                    9.4677e-11          102.98          8.6986          8.1663
m  eps_mean                     83.868      1.0447e+06           32448          4673.7
m  eps_var                      1587.2      6.8547e+11      9.3221e+08      6.6762e+07

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          44.926          5.8766          6.7668


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012935          26.074         0.70796         0.10795


  ** Temporal moment accumulated weights
     -----------------------------------

   id   n it.             value
   ---- -------- --------------
   0    109984          0.16002
   1    10                2e-05

 INSTANT    0.160022000E+00   TIME STEP NUMBER          110011
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160024000E+00   TIME STEP NUMBER          110012
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160026000E+00   TIME STEP NUMBER          110013
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160028000E+00   TIME STEP NUMBER          110014
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160030000E+00   TIME STEP NUMBER          110015
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160032000E+00   TIME STEP NUMBER          110016
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160034000E+00   TIME STEP NUMBER          110017
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160036000E+00   TIME STEP NUMBER          110018
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160038000E+00   TIME STEP NUMBER          110019
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160040000E+00   TIME STEP NUMBER          110020
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        8021        -0.643116256E-01
Smooth wall               5      295409        -0.132085019E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        8000         0.196404255E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37746E+02 0.14450E+02
   Friction velocity        uet   :  0.43987E-01 0.37373E+01
   Friction velocity        uk    :  0.43987E-01 0.37373E+01
   Dimensionless distance   yplus :  0.63085E-01 0.44961E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      48007
   Nb of faces within the viscous sub-layer     :     104419
   Total number of wall faces                   :     295409
------------------------------------------------------------



   ** INFORMATION ON UNSTEADY ROTOR/STATOR TREATMENT
      ----------------------------------------------
 Time dedicated to mesh update (s):      0.6530
 Global time                   (s):      0.6729

Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63330E+03     152   0.52253E-06   0.45744E+03 0.11557E+04 
c  Velocity[X]                                      0.16997E+03 
c  Velocity[Y]                                      0.11280E+03 
c  Velocity[Z]                                      0.17466E+03 
c  Pressure     0.11274E-01     128   0.25702E-03   0.12330E+00 0.70904E+04 
c  Turb Kinetic 0.14992E+03     137   0.93307E-08   0.10075E+03 0.22277E+04 
c  Turb Dissipa 0.23617E+06     117   0.88395E-08   0.28520E+11 0.80391E+04 
c  Tracer       0.43171E+01      52   0.48785E-06   0.15584E-02 0.51726E+03 
c  Variance_Tra 0.70687E-01      46   0.31910E-05   0.42398E-02 0.18100E+05 
-----------------------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy        -0.62275                          6162
a  Turb Dissipation            -1064.8                             1
a  Tracer                                            1                           5
a  Variance_Tracer          -3.484e-09                           129


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -28.357           28.64        -0.14381       -0.014459
v  Velocity[Y]                 -17.909           18.97         0.57868        0.072023
v  Velocity[Z]                 -28.012          28.604       -0.031868      0.00044738
v  ǁVelocityǁ                  0.01174          30.937          11.223          10.927
v  Pressure                  -5.62e+05      8.4103e+05      2.4704e+05      2.4003e+05
v  Turb Kinetic Energy       1.053e-08          37.209          2.8146          2.1049
v  Turb Dissipation         1.5946e-05       3.167e+06           29923          4186.1
v  Tracer                   1.1276e-15               1        0.026999        0.031824
v  Variance_Tracer                   0         0.97234      1.7548e-05       1.238e-05
v  Laminar Viscosity           0.01066         0.01066         0.01066         0.01066
v  Turb Viscosity           3.1991e-18          1.9292         0.13668         0.20433
v  CFL                      0.00013677          2.0706         0.11127        0.056432
v  Fourier Number           0.00025757          25.977         0.58597        0.050916
v  Total Pressure          -4.6068e+05      9.4235e+05      3.4837e+05      3.4135e+05
m  u_mean                       -14.55          14.794       -0.015224       -0.007904
m  v_mean                      -17.338          9.7255         0.67624        0.059738
m  w_mean                      -14.916          15.174       -0.007654     -0.00011102
m  Velocity_mean              0.019403          30.953          11.212          10.918
m  Velocity_variance        1.0393e-10          21.968        0.029078       0.0065756
m  uu_mean                  2.2087e-08          820.94          76.557            80.1
m  vv_mean                   9.457e-08          362.49          11.865          11.626
m  ww_mean                    5.68e-08          813.97          76.405          79.238
m  uv_mean                      -413.9          341.16       -0.028182        0.093009
m  uw_mean                     -404.74          378.25        -0.86239       -0.043606
m  vw_mean                        -350          269.18        0.045904        -0.12783
m  Wr_moy                          inf            -inf            -nan            -nan
m  Wt_moy                          inf            -inf            -nan            -nan
m  Wa_moy                            0               0               0               0
m  p_mean                  -6.5297e+05      9.8896e+05      2.3713e+05      2.2964e+05
m  k_mean                   9.1206e-06          13.435          3.2715          2.4869
m  k_var                    9.4695e-11          102.97           8.698          8.1657
m  eps_mean                      83.86      1.0446e+06           32447          4673.7
m  eps_var                      1588.8       6.854e+11      9.3219e+08       6.676e+07

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          44.961          5.8794          6.7694


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012474          26.459         0.69725         0.10735


  ** Temporal moment accumulated weights
     -----------------------------------

   id   n it.             value
   ---- -------- --------------
   0    109994          0.16004
   1    20                4e-05

 INSTANT    0.160042000E+00   TIME STEP NUMBER          110021
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160044000E+00   TIME STEP NUMBER          110022
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160046000E+00   TIME STEP NUMBER          110023
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160048000E+00   TIME STEP NUMBER          110024
 ============================================================= 


Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.
 INSTANT    0.160050000E+00   TIME STEP NUMBER          110025
 ============================================================= 



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

  max_time_step                          110025 (current: 110025)

 Finished reading "control_file".



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        8021        -0.643116256E-01
Smooth wall               5      295409        -0.132107904E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        8000         0.196427125E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36467E+02 0.14430E+02
   Friction velocity        uet   :  0.37319E-01 0.37377E+01
   Friction velocity        uk    :  0.37319E-01 0.37377E+01
   Dimensionless distance   yplus :  0.92412E-01 0.45000E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      48029
   Nb of faces within the viscous sub-layer     :     104422
   Total number of wall faces                   :     295409
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step     110025
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.Ang vel is 0.000000, rot axes are [0.000000, 0.000000, 0.000000]
.

 Write final restart files
   checkpoint at iteration     110025, Physical time    0.16005E+00


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

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

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

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


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



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


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





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




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


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

 Destroying structures and ending computation

