command: 
 ./cs_solver --param Calc

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

                                  (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:                Fr 17 Jan 2014 01:16:04 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/RPM2500/Case1/RESU/20140117-0116
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

  External libraries for partitioning:
    ParMETIS 4.0.3

 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   =             11 (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  =             31 (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)     )

   - SSG Rij-epsilon     (ITURB = 31)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       IRIJNU =              0 (Matrix stabilization        )
       IRIJRB =              0 (Reconstruct at boundaries   )
       IGRARI =              1 (Account for gravity         )
       ICLSYR =              1 (Symmetry implicitation      )
       ICLPTR =              0 (Wall implicitation          )

 --- 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))

   - SSG Rij-epsilon     (ITURB = 31)
       CSSGS1 =    0.17000E+01 (Cs1 coeff.                  )
       CSSGS2 =   -0.10500E+01 (Cs2 coeff.                  )
       CSSGR1 =    0.90000E+00 (Cr1 coeff.                  )
       CSSGR2 =    0.80000E+00 (Cr2 coeff.                  )
       CSSGR3 =    0.65000E+00 (Cr3 coeff.                  )
       CSSGR4 =    0.62500E+00 (Cr4 coeff.                  )
       CSSGR5 =    0.20000E+00 (Cr5 coeff.                  )
       CSRIJ  =    0.22000E+00 (Rij Cs diffusion coeff.     )
       CRIJ3  =    0.55000E+00 (Gravity term coeff.         )
       Ce1    =    0.14400E+01 (Ceps1 coeff.                )
       CSSGE2 =    0.18300E+01 (Ceps2 coeff.                )
       SIGMAE =    0.12200E+01 (sigma_eps coeff.            )
       CMU    =    0.90000E-01 (Cmu constant                )


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


 ** 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  =    0.10000E-03 (Minimum time step           )
       DTMAX  =    0.10000E+01 (Maximum time step           )
       DTREF  =    0.10000E-02 (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
 R11                   1  0.1000E+01
 R22                   1  0.1000E+01
 R33                   1  0.1000E+01
 R12                   1  0.1000E+01
 R13                   1  0.1000E+01
 R23                   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
 R11                   1      1      1      1      0 0.00E+00 0.10E+01
 R22                   1      1      1      1      0 0.00E+00 0.10E+01
 R33                   1      1      1      1      0 0.00E+00 0.10E+01
 R12                   1      1      1      1      0 0.00E+00 0.10E+01
 R13                   1      1      1      1      0 0.00E+00 0.10E+01
 R23                   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
 R11                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R22                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R33                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R12                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R13                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R23                 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
 R11                   1     -1  0.1500E+01
 R22                   1     -1  0.1500E+01
 R33                   1     -1  0.1500E+01
 R12                   1     -1  0.1500E+01
 R13                   1     -1  0.1500E+01
 R23                   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
 R11                  -1  10000  0.1000E-07      1
 R22                  -1  10000  0.1000E-07      1
 R33                  -1  10000  0.1000E-07      1
 R12                  -1  10000  0.1000E-07      1
 R13                  -1  10000  0.1000E-07      1
 R23                  -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
 R11                   0    100     10
 R22                   0    100     10
 R33                   0    100     10
 R12                   0    100     10
 R13                   0    100     10
 R23                   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 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 R11             
         7 R22             
         8 R33             
         9 R12             
        10 R13             
        11 R23             
        12 Dissip          
        15 TurbVisc        
        16 CourantNb       
        17 FourierNb       
        18 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 R11                           -1
         7 R22                           -1
         8 R33                           -1
         9 R12                           -1
        10 R13                           -1
        11 R23                           -1
        12 Dissip                        -1
        13 Density                       -1
        14 LamVisc                       -1
        15 TurbVisc                      -1
        16 CourantNb                     -1
        17 FourierNb                     -1
        18 total_pressure                -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 R11                            0
         7 R22                            0
         8 R33                            0
         9 R12                            0
        10 R13                            0
        11 R23                            0
        12 Dissip                         0
        15 TurbVisc                    -999
        16 CourantNb                   -999
        17 FourierNb                   -999
        18 total_pressure              -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: transient connectivity
      output: every 1 time steps and at calculation end


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

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

 Number of cells:                                      806998

 ----------------------------------------------------------
 Number of cells + halo cells:                         806998


 ----------------------------------------------------------
 Number of interior faces:                             1543726

 ----------------------------------------------------------
 Number of boundary faces:                             140540

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        511
      2 : [          3 ;          4 ] =     806487

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

 Writing file:        mesh_output
 Finished writing:    mesh_output

 Renumbering mesh:

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


 Matrix bandwidth for volume mesh :          717043
 Matrix profile/lines for volume mesh :      4681

 Mesh coordinates:               minimum    and maximum
                       X : -2.9997709e-02  1.0154000e-01
                       Y : -3.3797874e-02  2.9999820e-02
                       Z :  0.0000000e+00  6.9000000e-02
 Mesh
     Number of cells:          806998
     Number of interior faces: 1543726
     Number of boundary faces: 140540
     Number of vertices:       172424

 Groups:
    "Inlet"
       boundary faces:          144
    "Outlet"
       boundary faces:          156
    "Wall"
       boundary faces:       113824
    "boundary"
       boundary faces:        26416
    "cells"
       cells:                717688

 --- Information on the volumes
       Minimum control volume      =  2.5226492e-13
       Maximum control volume      =  2.5923329e-09
       Total volume for the domain =  3.0743025e-05

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

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 19186 -->   2 %

  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 (2.29 s)
  Global number of boundary faces selected for joining:      26416
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:        51189
    Vertex-Vertex intersections:            3455
    Other intersections:                   47734

  Global number of new vertices to create:      64477

  Equivalences broken for 7 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 40347 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 110 faces (global).
  Join mesh cleaning done.

  Edge removed for 110 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  =    0.31433E-01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  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
  R11               0.4000E-03  0.4000E-03
  R22               0.4000E-03  0.4000E-03
  R33               0.4000E-03  0.4000E-03
  R12               0.0000E+00  0.0000E+00
  R13               0.0000E+00  0.0000E+00
  R23               0.0000E+00  0.0000E+00
  Dissip            0.4208E-04  0.4208E-04
 ---------------------------------

  Local Time Step   0.1000E-02  0.1000E-02
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-02   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1035E+04  0.1035E+04
  LamVisc           0.3500E-02  0.3500E-02
  TurbVisc          0.7969E+00  0.7969E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         144
Smooth wall               5      113824
Rough wall                6           0
Symmetry                  4           0
Free outlet               3         156
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.10154E+00  -0.22208E-01   0.54206E-02



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         144         0.000000000E+00
Smooth wall               5      113824         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         156         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 0.48049E+01
   Friction velocity        uet   :  0.00000E+00 0.69546E+00
   Friction velocity        uk    :  0.21817E-02 0.97585E+00
   Dimensionless distance   yplus :  0.26256E-01 0.23176E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      20549
   Total number of wall faces                   :     113824
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ 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          1
@                                                            
@    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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

  Global number of boundary faces selected for joining:      26416
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:        52474
    Vertex-Vertex intersections:            3469
    Other intersections:                   49005

  Global number of new vertices to create:      65448

  Equivalences broken for 14 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 41241 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 138 faces (global).
  Join mesh cleaning done.

  Edge removed for 138 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):      2.4191
 Global time                   (s):      2.4775


   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14556E-01    3584   0.73393E+01   0.10912E+01 
c  VelocityX    0.61378E-02      43   0.54178E-01   0.27131E+05 
c  VelocityY    0.61378E-02      43   0.54178E-01   0.23767E+04 
c  VelocityZ    0.61378E-02      43   0.54178E-01   0.53838E+03 
c  R11          0.21880E-01    1774   0.31410E+00   0.37574E+00 
c  R22          0.21900E-01    1737   0.31380E+00   0.37724E+00 
c  R33          0.60985E-02    1825   0.24937E+00   0.10116E-01 
c  R12          0.25135E-01    1841   0.27661E+00   0.31957E-02 
c  R13          0.43251E-01    1720   0.40256E+00   0.12639E-02 
c  R23          0.43889E-01    1649   0.41221E+00   0.12317E-02 
c  Dissip       0.56721E+04    1689   0.30816E+00   0.42848E+11 
---------------------------------------------------------------
  
  

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

   field      initial min     initial max  clips to min  clips to max
-  ------  --------------  --------------  ------------  ------------
a  R11           -0.46184                        298205
a  R22           -0.41844                        316399
a  R33           -0.26257                        170834
a  R12           -0.52432                        638503
a  R13           -0.41083                        681288
a  R23           -0.42853                        677561
a  Dissip


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                811.28      1.3147e+06      1.2253e+06      1.0093e+06
v  Velocity[x]            -84.028          155.35          1.4525             2.4
v  Velocity[y]            -181.41          9.8832         -1.1035          -0.604
v  Velocity[z]            -63.102          64.884         0.14474       -0.019417
v  R11                 5.5838e-08         0.41924        0.021975       0.0041773
v  R22                 3.7912e-09         0.46264        0.022298       0.0040795
v  R33                 5.7337e-09         0.27002       0.0038535       0.0006783
v  R12                  -0.016952        0.013805     -3.3779e-05     -4.0233e-05
v  R13                  -0.094589        0.098824      2.6546e-05      2.6957e-05
v  R23                   -0.13915        0.085364     -4.4001e-05      1.9779e-05
v  Dissip              4.2075e-05      2.5983e+05           17050          2515.2
v  TurbVisc               0.79691         0.79691         0.79691         0.79691
v  CourantNb                    0               0               0               0
v  FourierNb               3.0433          1720.5           313.6          45.129
v  total_pressure      1.0214e+05      1.4161e+06      1.3266e+06      1.1106e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.0433          1720.5           313.6          45.127


 TIME FOR THE TIME STEP                1:        0.70008E+03

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


 INSTANT    0.200000000E-02   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         144        -0.431250000E-01
Smooth wall               5      113824        -0.724271671E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         156         0.767383917E+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 0.10013E+03
   Friction velocity        uet   :  0.23449E-02 0.91764E+01
   Friction velocity        uk    :  0.88466E-02 0.24723E+01
   Dimensionless distance   yplus :  0.42659E+00 0.49351E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1930
   Total number of wall faces                   :     113824
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ 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          2
@                                                            
@    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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

  Global number of boundary faces selected for joining:      26416
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:        51628
    Vertex-Vertex intersections:            3250
    Other intersections:                   48378

  Global number of new vertices to create:      65036

  Equivalences broken for 17 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 40752 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 122 faces (global).
  Join mesh cleaning done.

  Edge removed for 122 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):      2.4036
 Global time                   (s):      2.4632


   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.87425E-01    3440   0.19788E+01   0.16905E+01 
c  VelocityX    0.33919E+01     751   0.90464E+00   0.20479E+05 
c  VelocityY    0.33919E+01     751   0.90464E+00   0.22274E+04 
c  VelocityZ    0.33919E+01     751   0.90464E+00   0.40999E+03 
c  R11          0.18615E+00     115   0.40382E-04   0.12504E+00 
c  R22          0.19063E+00     114   0.40713E-04   0.12639E+00 
c  R33          0.62320E-01     137   0.34343E-04   0.39288E-02 
c  R12          0.52963E-01     105   0.39872E-04   0.19044E-02 
c  R13          0.36062E-01     140   0.75163E-04   0.54334E-03 
c  R23          0.34017E-01     139   0.80773E-04   0.52558E-03 
c  Dissip       0.19237E+04     107   0.29961E-02   0.41975E+11 
---------------------------------------------------------------
  
  

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

   field      initial min     initial max  clips to min  clips to max
-  ------  --------------  --------------  ------------  ------------
a  R11         -0.0086266                         15406
a  R22         -0.0096235                         17052
a  R33         -0.0068254                         28889
a  R12          -0.047243                        288343
a  R13           -0.04178                        250792
a  R23          -0.057054                        271023
a  Dissip         -4885.3                        152377


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                685.78      1.6053e+06      1.5032e+06      1.2151e+06
v  Velocity[x]            -187.74          274.37          2.5222          4.4544
v  Velocity[y]            -370.55          16.655         -2.2356         -1.1553
v  Velocity[z]            -129.82          123.86         0.36299        0.033344
v  R11                 1.5287e-09         0.21447       0.0096344       0.0017959
v  R22                 6.6269e-09         0.21054       0.0097243       0.0017558
v  R33                 1.8875e-09         0.11545       0.0019398      0.00034649
v  R12                  -0.047243        0.057028      6.9986e-05     -2.1609e-06
v  R13                  -0.038695        0.048363     -1.2778e-05      5.1349e-07
v  R23                  -0.054728        0.036572     -9.5508e-06     -2.6998e-06
v  Dissip              2.4283e-05           34707          286.55          17.277
v  TurbVisc             4.823e-15         0.74737       0.0074224        0.052168
v  CourantNb             0.014505            2863          68.261          19.298
v  FourierNb             0.013272          34.533          1.6193          1.3511
v  total_pressure      1.0201e+05      1.7067e+06      1.6045e+06      1.3164e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.032073          2864.7           69.88          20.648


 TIME FOR THE TIME STEP                2:        0.38267E+03

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


 INSTANT    0.300000000E-02   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         144        -0.431250000E-01
Smooth wall               5      113824        -0.137200006E+01
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         156         0.141512532E+01
Free inlet               13           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 0.18400E+03
   Friction velocity        uet   :  0.74307E-02 0.15777E+02
   Friction velocity        uk    :  0.12958E-01 0.33713E+01
   Dimensionless distance   yplus :  0.43028E+00 0.67660E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2664
   Total number of wall faces                   :     113824
------------------------------------------------------------


  Global number of boundary faces selected for joining:      26416
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:        51034
    Vertex-Vertex intersections:            3295
    Other intersections:                   47739

  Global number of new vertices to create:      64236

  Equivalences broken for 8 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 40233 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 104 faces (global).
  Join mesh cleaning done.

  Edge removed for 104 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):      2.3085
 Global time                   (s):      2.3674

SIGFPE signal (floating point exception) intercepted!

Call stack:
   1: 0x7715c4     <>                               (cs_solver)
   2: 0x834fa5     <>                               (cs_solver)
   3: 0x82fec7     <>                               (cs_solver)
   4: 0x6e2d1a     <>                               (cs_solver)
   5: 0x430677     <>                               (cs_solver)
   6: 0x431356     <>                               (cs_solver)
   7: 0x6d3b7c     <>                               (cs_solver)
   8: 0x45fdbe     <>                               (cs_solver)
   9: 0x438abb     <>                               (cs_solver)
  10: 0x43562d     <>                               (cs_solver)
  11: 0x413739     <>                               (cs_solver)
  12: 0x40f0d5     <>                               (cs_solver)
  13: 0x405e63     <>                               (cs_solver)
  14: 0x7f122bb9176d <__libc_start_main+0xed>         (libc.so.6)
  15: 0x405ea5     <>                               (cs_solver)
End of stack

