command: 
 /opt/saturne-3.0/libexec/code_saturne/cs_solver --param LES.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.0.0


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

  build Thu 02 May 2013 08:06:16 AM PKT
  MPI version 2.1 (Open MPI 1.4.3)


  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:                Sun 05 Jun 2016 10:35:20 AM PKT
  System:              Linux 3.2.0-60-generic
  Machine:             fahad-virtual-machine
  Processor:           model name	: AMD Opteron(tm) Processor 6348
  Memory:              122453 MB
  User:                fahad (Fahad)
  Directory:           /home/fahad/Desktop/Code_Saturne_CircularCylinder/CIRCULARCYLINDER/LES/RESU/20160605-1031
  MPI ranks:           12 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    ParMETIS 3.1
    PT-SCOTCH 1.12.2147483631

 Reading metadata from file: "mesh_input"

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

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


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



@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@
@ @@   WARNING :      WHEN READING INPUT DATA
@    =========
@   CHOICE OF TIME-SCHEME
@
@     TIME-SCHEME FOR VELOCITY IS SECOND ORDER
@       (THETAV =   0.50E+00)
@     CERTAIN TERMES ARE HOWEVER FIRST ORDER IN TIME  WITH
@       THE FOLLOWING SETTINGS:
@
@ parameters       ISTMPF ISNO2T ISTO2T IROEXT IVIEXT ICPEXT
@ Values  entered      2      1      0      0      0      0
@
@  computation will go on.
@
@ Check the input data given through the User Interface
@   or in cs_user_parameters.f90.
@
@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@


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


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

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

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


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

 --- Geometry
       NPRFML =              1 (Nb max. family properties   )
       NFML   =              7 (Nb families                 )

 --- Physics
       NVAR   =              4 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              9 (Nb cell properties          )
       NPROFA =              2 (Nb internal face properties )
       NPROFB =              3 (Nb boundary face properties )


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


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

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

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

  -- Continuous phase:

       RO0    =    0.11786E+01 (Reference density           )
       VISCL0 =    0.18300E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             40 (Turbulence model            )
       IDEUCH =              0 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.10880E+02 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )
       ISCALT =             -1 (Temperature salar number    )

   - LES                 (ITURB = 40, 41, 42)
                               (Sub-grid scale model        )
                               (40 Smagorinsky model        )
                               (41 Dynamic model            )
                               (42 WALE model               )
       CSMAGO =    0.65000E-01 (Smagorinsky constant        )
       CWALE  =    0.25000E+00 (WALE model constant         )
       XLESFL =    0.20000E+01 (Filter with in a cell is    )
       ALES   =    0.10000E+01 (written as                  )
       BLES   =    0.33333E+00 (XLESFL*(ALES*VOLUME)**(BLES))
       IDRIES =              1 (=1 Van Driest damping       )
       CDRIES =    0.26000E+02 (Van Driest constant         )
       XLESFD =    0.15000E+01 (Ratio between the explicit  )
                               (filter and LES filter       )
                               (recommended value: 1.5      )
       SMAGMX =    0.65000E+00 (Max Smagonsky in the        )
                               (dynamic model case          )
       IVRTEX =              0 (Use the vortex method       )
 --- 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))


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


 ** 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-04 (Minimum time step           )
       DTMAX  =    0.10000E+00 (Maximum time step           )
       DTREF  =    0.10000E-03 (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
----------------------------

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

 --- Order of base time stepping scheme
       ISCHTP =              2 (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      1 0.10E+01 0.50E+00
 VelocityY             1      1      1      1      1 0.10E+01 0.50E+00
 VelocityZ             1      1      1      1      1 0.10E+01 0.50E+00
-------------------------------------------------------------

       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
    ------
       IVELCO =              1 (0: segregated solving of the
                                   velocity components during
                                   the prediction step
                                1: coupled solving of the
                                   velocity components       )
       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 =              2 (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 =              2 (time scheme for flow
                               (0: explicit (THETFL = 0     )
                               (1: std scheme (Saturne 1.0  )
                               (2: 2nd-order (THETFL = 0.5  )
       THETFL =    0.50000E+00 (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 =    0.50000E+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      5  0.1000E-04  0.1000E-03  0.0000E+00
 VelocityX           100     10  0.1000E-04  0.1000E-03  0.0000E+00
 VelocityY           100     10  0.1000E-04  0.1000E-03  0.0000E+00
 VelocityZ           100     10  0.1000E-04  0.1000E-03  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
-----------------------------------

       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           )

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


 ** WALL DISTANCE COMPUTATION
    -------------------------

       ICDPAR =             -1 ( 1: std, reread if restart
                               (-1: std, recomputed if restrt
                               ( 2: old, reread if restart
                               (-2: old, recomputed if restrt


       NITMAY =          10000 (Nb iter for iter resolution )
       NSWRSY =              1 (Nb iter for rhs reconstr.   )
       NSWRGY =            100 (Nb iter for grad. reconstr. )
       IMLIGY =             -1 (Gradient limitation method  )
       IRCFLY =              1 (Conv. Diff. flow reconstr.  )
       ISCHCY =              1 (Convective scheme           )
       ISSTPY =              0 (Slope tet use               )
       IMGRPY =              0 (Multigrid algorithm         )
       IWARNY =              0 (Verbosity level             )
       NTCMXY =           1000 (Nb iter for steady convect. )

       BLENCY =    0.00000E+00 (2nd order conv. scheme prop.)
       EPSILY =    0.10000E-07 (Iterative solver precision  )
       EPSRSY =    0.10000E-04 (rhs reconstruction precision)
       EPSRGY =    0.10000E-04 (Gradient reconstr. precision)
       CLIMGY =    0.15000E+01 (Coeff. for grad. limitation )
       EXTRAY =    0.00000E+00 (Coeff. for grad. extrapolat.)
       COUMXY =    0.50000E+04 (Max CFL for convection      )
       EPSCVY =    0.10000E-07 (Precision for steady conv.  )
       YPLMXY =    0.20000E+03 (y+ max w. damping influence )


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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Pressure              0  10000  0.1000E-04      1
 VelocityX            -1  10000  0.1000E-04      1
 VelocityY            -1  10000  0.1000E-04      1
 VelocityZ            -1  10000  0.1000E-04      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
------------------------------

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


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

  Multigrid coarsening type: algebraic, face traveral by criteria

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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =             10 (Final time step required    )

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


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


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

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

 --- Post-processed variables

       Number Name
         2 Pressure        
         3 VelocityX       
         4 VelocityY       
         5 VelocityZ       
         9 CourantNb       
        10 FourierNb       
        11 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 Density                       -1
         7 LamVisc                       -1
         9 CourantNb                     -1
        10 FourierNb                     -1
        11 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
         9 CourantNb                   -999
        10 FourierNb                   -999
        11 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)


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


 Reading file:        mesh_input
 Finished reading:    mesh_input
 No "partition_input/domain_number_12" file available;

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

 Partitioning 11275730 cells to 12 domains
  (METIS_PartGraphKway).

  Total number of faces on parallel boundaries: 4528
  wall-clock time: 16.922228 s

  Number of cells per domain (histogramm):
    [     938292 ;     938533 [ =          1
    [     938533 ;     938775 [ =          0
    [     938775 ;     939017 [ =          1
    [     939017 ;     939259 [ =          1
    [     939259 ;     939501 [ =          3
    [     939501 ;     939743 [ =          1
    [     939743 ;     939985 [ =          0
    [     939985 ;     940227 [ =          2
    [     940227 ;     940469 [ =          2
    [     940469 ;     940711 ] =          1

 Writing file:        partition_output/domain_number_12
 Finished writing:    partition_output/domain_number_12

 Partitioning finished (37.3 s)


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: every 1 time steps


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

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

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

 Histogram of the number of cells per rank:

    minimum value =             938292
    maximum value =             940711

      1 : [     938292 ;     938775 [ =          1
      2 : [     938775 ;     939259 [ =          2
      3 : [     939259 ;     939743 [ =          4
      4 : [     939743 ;     940227 [ =          2
      5 : [     940227 ;     940711 ] =          3

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

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

    minimum value =             939343
    maximum value =             941489

      1 : [     939343 ;     939772 [ =          2
      2 : [     939772 ;     940201 [ =          5
      3 : [     940201 ;     940630 [ =          0
      4 : [     940630 ;     941059 [ =          2
      5 : [     941059 ;     941489 ] =          3

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

 Histogram of the number of ghost cells per rank:

    minimum value =                576
    maximum value =               1051

      1 : [        576 ;        671 [ =          5
      2 : [        671 ;        766 [ =          2
      3 : [        766 ;        861 [ =          2
      4 : [        861 ;        956 [ =          1
      5 : [        956 ;       1051 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =            1404178
    maximum value =            1407117

      1 : [    1404178 ;    1404765 [ =          1
      2 : [    1404765 ;    1405353 [ =          5
      3 : [    1405353 ;    1405941 [ =          2
      4 : [    1405941 ;    1406529 [ =          2
      5 : [    1406529 ;    1407117 ] =          2

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

 Histogram of the number of boundary faces per rank:

    minimum value =            1884155
    maximum value =            1891263

      1 : [    1884155 ;    1885576 [ =          1
      2 : [    1885576 ;    1886998 [ =          4
      3 : [    1886998 ;    1888419 [ =          3
      4 : [    1888419 ;    1889841 [ =          2
      5 : [    1889841 ;    1891263 ] =          2

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  3

      1 : [          2 ;          3 ] =   11275730

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  2
    maximum value =                  5

      1 : [          2 ;          3 [ =          3
      2 : [          3 ;          4 [ =          4
      3 : [          4 ;          5 ] =          5

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

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

 Renumbering mesh:

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


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =             938285
    maximum value =             940609

      1 : [     938285 ;     938749 [ =          1
      2 : [     938749 ;     939214 [ =          3
      3 : [     939214 ;     939679 [ =          3
      4 : [     939679 ;     940144 [ =          1
      5 : [     940144 ;     940609 ] =          4

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =                  9
    maximum value =               4256

      1 : [          9 ;        858 [ =          3
      2 : [        858 ;       1707 [ =          2
      3 : [       1707 ;       2557 [ =          0
      4 : [       2557 ;       3406 [ =          2
      5 : [       3406 ;       4256 ] =          5

 Mesh coordinates:               minimum    and maximum
                       X : -7.0000000e+00  1.5000000e+01
                       Y : -5.0000000e+00  5.0000000e+00
                       Z :  0.0000000e+00  1.0000000e+00
 Mesh
     Number of cells:          11275730
     Number of interior faces: 16863169
     Number of boundary faces: 22652312
     Number of vertices:       11376582

 Groups:
    "Back"
       boundary faces:     11275730
    "Bottom"
       boundary faces:          275
    "Front"
       boundary faces:     11275730
    "Left"
       boundary faces:          125
    "Top"
       boundary faces:          275
    "right"
       boundary faces:          125

 --- Information on the volumes
       Minimum control volume      =  5.5578274e-11
       Maximum control volume      =  5.2654104e-03
       Total volume for the domain =  2.1685841e+02

  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: 2113 -->   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 (4.95 s)
                                                             
       ALMAX  =    0.59972E+01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.


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


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

  Local Time Step   0.1000E-03  0.1000E-03
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-03   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  Density           0.1179E+01  0.1179E+01
  LamVisc           0.1830E-04  0.1830E-04
  Turb Viscosity    0.0000E+00  0.0000E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         125
Smooth wall               5           0
Rough wall                6      100052
Symmetry                  4    22552010
Free outlet               3         125
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.15000E+02   0.61542E-11   0.50000E+00



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         125         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6      100052         0.000000000E+00
Symmetry                  4    22552010         0.000000000E+00
Free outlet               3         125         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14672E-11 0.93805E-10
   Friction velocity        uk    :  0.14672E-11 0.93805E-10
   Rough dimensionless dist yplus :  0.44874E-02 0.33143E+00
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------


                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.44965E-06 Max distance =    0.15965E+02
                                                             
     (Distance calculation done in       7146 iterations)



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         125        -0.785746667E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6      100052         0.000000000E+00
Symmetry                  4    22552010         0.000000000E+00
Free outlet               3         125         0.785412369E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14672E-11 0.93805E-10
   Friction velocity        uk    :  0.14672E-11 0.93805E-10
   Rough dimensionless dist yplus :  0.44874E-02 0.33143E+00
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24368E+01     240   0.15038E-04   0.23125E+00 
c  VelocityX    0.75714E+05       2   0.45212E-04   0.10353E+07 
c  VelocityY    0.75714E+05       2   0.45212E-04   0.72629E+04 
c  VelocityZ    0.75714E+05       2   0.45212E-04   0.15070E-23 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure     0.11442E+04   0.26693E+07         --         -- 
v  VelocityX   -0.10198E+02   0.25969E+02         --         -- 
v  VelocityY   -0.15012E+02   0.14817E+02         --         -- 
v  VelocityZ   -0.12273E-12   0.12082E-12         --         -- 
v  CourantNb    0.00000E+00   0.00000E+00          0          0 
v  FourierNb    0.17084E-05   0.17161E+03          0          0 
v  total_pressu 0.10247E+06   0.27706E+07          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.38297E-01  0.99929E+00  0.50000E+00  
Courant max  0.00000E+00  0.38297E-01  0.99929E+00  0.50000E+00  
Fourier min  0.17084E-05 -0.48000E+01 -0.49794E+01  0.50000E+00  
Fourier max  0.17161E+03 -0.90219E+00 -0.43133E+00  0.50000E+00  
Cou_Fou min  0.17084E-05 -0.48000E+01 -0.49794E+01  0.50000E+00  
Cou_Fou max  0.17161E+03 -0.90219E+00 -0.43133E+00  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                1:        0.25943E+04

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


