command: 
 /home/caelinux/opt/code_saturne-3.2.1/arch/Linux_x86_64/libexec/code_saturne/cs_solver --param Calc

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

                                  (R)
                      Code_Saturne

                      Version 3.2.1


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

  build Fr 13 Dez 2013 14:02:19 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:                Di 17 Dez 2013 21:21:08 CET
  System:              Linux 3.8.0-30-generic
  Machine:             caelinux-VirtualBox
  Processor:           model name	: Intel(R) Core(TM) i7-2675QM CPU @ 2.20GHz
  Memory:              8375 MB
  User:                caelinux (caelinux)
  Directory:           /home/caelinux/opt/code_saturne-3.2.1/arch/Linux_x86_64/bin/Joining/Case1/RESU/20131217-2120
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

  External libraries for partitioning:
    METIS

 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   =              4 (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    =    0.11786E+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

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


 ** 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  =              0 (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 =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

 --- 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 =              2 (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-01 (Minimum time step           )
       DTMAX  =    0.10000E+03 (Maximum time step           )
       DTREF  =    0.10000E+00 (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 =              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
-------------------------------------------------------------

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

-------------------------------------------
 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           )

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


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

       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 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       
         8 CourantNb       
         9 FourierNb       
        10 total_pressure  
        11 LocalTime       
         --           --

 --- 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
         8 CourantNb                     -1
         9 FourierNb                     -1
        10 total_pressure                -1
        11 LocalTime                     -1
         --           --                --

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

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

         2 Pressure                       0
         3 VelocityX                      0
         4 VelocityY                      0
         5 VelocityZ                      0
         8 CourantNb                   -999
         9 FourierNb                   -999
        10 total_pressure              -999
        11 LocalTime                   -999
         --           --                --

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


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


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

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


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


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

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


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

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


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

  Selection criteria: "coupled_boundary"

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

  Advanced joining parameters:
    Verbosity level:                                 1
    Visualization level:                             1
    Deepest level reachable in tree building:       30
    Max boxes by leaf:                              25
    Max ratio of linked boxes / init. boxes:   5.00000
    Max ratio of boxes for distribution:       2.00000
    Merge step tolerance multiplier:           1.00000
    Pre-merge factor:                          0.05000
    Tolerance computation mode:                      1
    Intersection computation mode:                   1
    Max. number of equiv. breaks:                  500
    Max. number of subfaces by face:               200

  Before joining
     Number of cells:          1624991
     Number of interior faces: 3157166
     Number of boundary faces: 185632
     Number of vertices:       323269

  Global number of boundary faces selected for joining:      25602

  Element selection successfully done.
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:        38095
    Vertex-Vertex intersections:            1463
    Other intersections:                   36632

  Joining operation is non-conforming.

  Global number of new vertices to create:      53949

  Equivalences broken for 9 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 30347 global element couples.

  Max size of a merge set of vertices: 8

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 65 faces (global).
  Join mesh cleaning done.

  Edge removed for 65 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  *** WARNING ***
  Globally, 22 problem(s) found during the face splitting
                0  open cycles,
               22  edges traversed twice,
                0  faces split into more than max_subfaces (= 200)

    => Eventually modify joining parameters


  Global number of faces after splitting:      44220

  Global configuration after the joining operation:
     Global number of border faces to add:        372

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

  After joining
     Number of cells:          1624991
     Number of interior faces: 3201014
     Number of boundary faces: 160402
     Number of vertices:       340428


  Joining  1 completed (1.82 s).

  All joining operations successfully finished:

    Wall clock time:                  1.82

 Number of cells:                                      1624991

 ----------------------------------------------------------
 Number of cells + halo cells:                         1624991


 ----------------------------------------------------------
 Number of interior faces:                             3201014

 ----------------------------------------------------------
 Number of boundary faces:                             160402

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                 87

      1 : [          2 ;         19 [ =    1624175
      2 : [         19 ;         36 [ =        590
      3 : [         36 ;         53 [ =        137
      4 : [         53 ;         70 [ =         71
      5 : [         70 ;         87 ] =         18

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

 Writing file:        mesh_output
 Finished writing:    mesh_output
 Number of cells:                                      1624991

 ----------------------------------------------------------
 Number of cells + halo cells:                         1624991


 ----------------------------------------------------------
 Number of interior faces:                             3201014

 ----------------------------------------------------------
 Number of boundary faces:                             160402

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                 87

      1 : [          2 ;         19 [ =    1624175
      2 : [         19 ;         36 [ =        590
      3 : [         36 ;         53 [ =        137
      4 : [         53 ;         70 [ =         71
      5 : [         70 ;         87 ] =         18

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

 Renumbering mesh:

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


 Matrix bandwidth for volume mesh :          1599695
 Matrix profile/lines for volume mesh :      1952

 Mesh coordinates:               minimum    and maximum
                       X : -2.9999653e+01  6.1540000e+01
                       Y : -3.3797720e+01  2.9999969e+01
                       Z :  0.0000000e+00  2.9000000e+01
 Mesh
     Number of cells:          1624991
     Number of interior faces: 3201014
     Number of boundary faces: 160402
     Number of vertices:       340428

 Groups:
    "Inlet"
       boundary faces:           46
    "Outlet"
       boundary faces:           58
    "coupled_boundary"
       interior faces:        43848
       boundary faces:          372
    "wall"
       boundary faces:       159926

 --- Information on the volumes
       Minimum control volume      =  3.8581768e-08
       Maximum control volume      =  1.3163104e+01
       Total volume for the domain =  2.1711937e+04

  Criterion 1: Orthogonality:
    Number of bad cells detected: 974 -->   0 %

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 39746 -->   2 %

  Criterion 4: Cells Volume Ratio:
    Number of bad cells detected: 2660 -->   0 %

  Criterion 5: Guilt by Association:
    Number of bad cells detected: 8 -->   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 (5.45 s)
                                                             
       ALMAX  =    0.27805E+02 (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
 ---------------------------------

  LocalTime         0.1000E+00  0.1000E+00
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E+00   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  LamVisc           0.1830E-04  0.1830E-04
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          46
Smooth wall               5      159926
Rough wall                6           0
Symmetry                  4         372
Free outlet               3          58
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


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



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46         0.000000000E+00
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.00000E+00 0.00000E+00
   Dimensionless distance   yplus :  0.00000E+00 0.00000E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56648E+02    3584   0.13751E+01   0.95764E+00 
c  VelocityX    0.19505E-02       3   0.23115E-05   0.53621E+02 
c  VelocityY    0.19505E-02       3   0.23115E-05   0.71776E+01 
c  VelocityZ    0.19505E-02       3   0.23115E-05   0.10213E+02 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                7.2572          5597.9          4442.6          4055.8
v  Velocity[x]            -85.649          146.75          3.6282         0.90299
v  Velocity[y]            -168.36          6.1393          -4.611        -0.35971
v  Velocity[z]            -70.885          77.564         0.44369        -0.32682
v  CourantNb                    0               0               0               0
v  FourierNb           3.5704e-06          1.3682        0.028422      0.00014162
v  total_pressure      1.0133e+05      1.0692e+05      1.0577e+05      1.0538e+05
v  LocalTime                 0.11            0.11            0.11            0.11


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      3.5704e-06          1.3682        0.028422      0.00014162


 TIME FOR THE TIME STEP                1:        0.54768E+03

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


 INSTANT    0.200000000E+00   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391815707E+03
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 0.00000E+00
   Friction velocity        uet   :  0.41773E-03 0.10960E+01
   Friction velocity        uk    :  0.41773E-03 0.10960E+01
   Dimensionless distance   yplus :  0.50235E+01 0.67332E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71992E+02    3431   0.58104E+00   0.19421E+01 
c  VelocityX    0.83883E+04     124   0.30313E-01   0.16080E+01 
c  VelocityY    0.83883E+04     124   0.30313E-01   0.70008E+00 
c  VelocityZ    0.83883E+04     124   0.30313E-01   0.53844E+00 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime      1.2345e-05                        687084


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1639.7          531.34          406.05          418.54
v  Velocity[x]            -75.801          82.511          2.8595         0.91631
v  Velocity[y]            -127.37           8.765         -3.9817        -0.39751
v  Velocity[z]            -72.559           81.26         0.46718        -0.33548
v  CourantNb           0.00061222          810.04          9.8241         0.45788
v  FourierNb           3.9274e-06         0.12438       0.0029406      0.00011388
v  total_pressure           99685      1.0186e+05      1.0173e+05      1.0174e+05
v  LocalTime                 0.01           0.121        0.052135         0.11323


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00062261          810.08           9.827           0.458


 TIME FOR THE TIME STEP                2:        0.55645E+03

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


 INSTANT    0.300000000E+00   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391810689E+03
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 0.00000E+00
   Friction velocity        uet   :  0.44153E-03 0.87362E+00
   Friction velocity        uk    :  0.44153E-03 0.87362E+00
   Dimensionless distance   yplus :  0.36240E+01 0.67727E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.36413E+02    3339   0.50565E+00   0.10046E+01 
c  VelocityX    0.83523E+04     117   0.43089E-01   0.77657E+00 
c  VelocityY    0.83523E+04     117   0.43089E-01   0.41890E+00 
c  VelocityZ    0.83523E+04     117   0.43089E-01   0.19643E+00 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime      1.7848e-05                        688097


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2411.5          422.39          292.39          339.15
v  Velocity[x]            -75.945          43.605          2.3752         0.92668
v  Velocity[y]            -101.05          12.006         -3.5958        -0.41781
v  Velocity[z]            -62.779          65.353         0.48489        -0.33768
v  CourantNb            0.0001848           560.3          7.9685         0.48881
v  FourierNb           4.3202e-06         0.12438       0.0029498      0.00012045
v  total_pressure           98913      1.0175e+05      1.0162e+05      1.0166e+05
v  LocalTime                 0.01          0.1331        0.054119         0.12282


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00019623          560.34          7.9715         0.48893


 TIME FOR THE TIME STEP                3:        0.50172E+03

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


 INSTANT    0.400000000E+00   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391810689E+03
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 0.00000E+00
   Friction velocity        uet   :  0.49195E-03 0.77754E+00
   Friction velocity        uk    :  0.49195E-03 0.77754E+00
   Dimensionless distance   yplus :  0.43397E+01 0.68855E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.30853E+02    2895   0.73006E+00   0.75785E+00 
c  VelocityX    0.83099E+04     111   0.50637E-01   0.64798E+00 
c  VelocityY    0.83099E+04     111   0.50637E-01   0.33829E+00 
c  VelocityZ    0.83099E+04     111   0.50637E-01   0.15451E+00 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime      2.1751e-05                        688693


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2478.6          338.95          209.95          274.58
v  Velocity[x]            -55.322          34.504          1.9712         0.92925
v  Velocity[y]            -79.855          21.972         -3.3675        -0.42245
v  Velocity[z]            -53.827          58.477         0.51177        -0.33919
v  CourantNb           0.00057722          459.76          6.9179         0.51844
v  FourierNb           4.7522e-06         0.12438       0.0029641      0.00012806
v  total_pressure           98846      1.0166e+05      1.0153e+05       1.016e+05
v  LocalTime                 0.01         0.14641        0.056658         0.13326


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00058979          459.79          6.9208         0.51857


 TIME FOR THE TIME STEP                4:        0.47352E+03

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


 INSTANT    0.500000000E+00   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391810796E+03
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 0.00000E+00
   Friction velocity        uet   :  0.54852E-03 0.71708E+00
   Friction velocity        uk    :  0.54852E-03 0.71708E+00
   Dimensionless distance   yplus :  0.42751E+01 0.70800E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.44041E+02    1151   0.11890E+01   0.92405E+00 
c  VelocityX    0.82765E+04     117   0.44089E-01   0.61299E+00 
c  VelocityY    0.82765E+04     117   0.44089E-01   0.41728E+00 
c  VelocityZ    0.82765E+04     117   0.44089E-01   0.17967E+00 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime       2.337e-05                        689159


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2098.1          320.96          197.13          262.43
v  Velocity[x]            -104.54          35.692          1.4683         0.92918
v  Velocity[y]             -60.19          45.315         -3.0259        -0.42106
v  Velocity[z]             -50.76           62.91         0.55337        -0.34077
v  CourantNb           0.00095097          427.91          6.4686         0.54759
v  FourierNb           5.2274e-06         0.12438       0.0029806      0.00013649
v  total_pressure           99227      1.0165e+05      1.0152e+05      1.0159e+05
v  LocalTime                 0.01         0.16105        0.059539         0.14455


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0009648          427.94          6.4716         0.54773


 TIME FOR THE TIME STEP                5:        0.23435E+03

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


 INSTANT    0.600000000E+00   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391810710E+03
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 0.00000E+00
   Friction velocity        uet   :  0.49377E-03 0.78830E+00
   Friction velocity        uk    :  0.49377E-03 0.78830E+00
   Dimensionless distance   yplus :  0.32427E+01 0.71402E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.82937E+02    1507   0.19196E+01   0.13115E+01 
c  VelocityX    0.82703E+04     152   0.40552E-01   0.48756E+00 
c  VelocityY    0.82703E+04     152   0.40552E-01   0.48718E+00 
c  VelocityZ    0.82703E+04     152   0.40552E-01   0.15326E+00 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime      2.7625e-05                        689479


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1829.2          319.64          197.16          260.28
v  Velocity[x]            -66.908          35.645          1.3251         0.92885
v  Velocity[y]            -55.276          55.283         -2.4869        -0.41916
v  Velocity[z]            -53.226          57.355          0.5399        -0.34316
v  CourantNb            0.0010098          361.98          6.6785         0.57647
v  FourierNb           5.3306e-06         0.12438       0.0029967      0.00014534
v  total_pressure           99496      1.0164e+05      1.0152e+05      1.0159e+05
v  LocalTime                 0.01         0.17716        0.062499         0.15658


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001025          362.02          6.6815         0.57662


 TIME FOR THE TIME STEP                6:        0.28251E+03

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


 INSTANT    0.700000000E+00   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391810680E+03
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 0.00000E+00
   Friction velocity        uet   :  0.54901E-03 0.68459E+00
   Friction velocity        uk    :  0.54901E-03 0.68459E+00
   Dimensionless distance   yplus :  0.35416E+01 0.71035E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.17794E+03    3007   0.25602E+01   0.16813E+01 
c  VelocityX    0.82797E+04     156   0.39885E-01   0.43147E+00 
c  VelocityY    0.82797E+04     156   0.39885E-01   0.31244E+00 
c  VelocityZ    0.82797E+04     156   0.39885E-01   0.22187E+00 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime       3.285e-05                        689896


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                 -1636          318.52           197.5          257.72
v  Velocity[x]            -49.508          34.865          1.3911         0.92888
v  Velocity[y]            -51.331          55.706         -2.1544        -0.41793
v  Velocity[z]            -47.203          51.316         0.51871        -0.34819
v  CourantNb           0.00086459          304.42          6.5731         0.60543
v  FourierNb           5.3306e-06         0.12438       0.0030109      0.00015432
v  total_pressure           99689      1.0164e+05      1.0152e+05      1.0158e+05
v  LocalTime                 0.01         0.19487        0.065356         0.16926


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00088133          304.45          6.5761         0.60558


 TIME FOR THE TIME STEP                7:        0.49877E+03

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


 INSTANT    0.800000000E+00   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391810505E+03
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 0.00000E+00
   Friction velocity        uet   :  0.51015E-03 0.55475E+00
   Friction velocity        uk    :  0.51015E-03 0.55475E+00
   Dimensionless distance   yplus :  0.31431E+01 0.71584E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.38269E+03    1862   0.29933E+01   0.19077E+01 
c  VelocityX    0.83137E+04     161   0.39749E-01   0.44224E+00 
c  VelocityY    0.83137E+04     161   0.39749E-01   0.21353E+00 
c  VelocityZ    0.83137E+04     161   0.39749E-01   0.56594E+00 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime      3.9341e-05                        690227


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1639.6           312.7          189.93          247.73
v  Velocity[x]             -46.36          34.244          1.5136         0.92914
v  Velocity[y]            -47.169          51.514         -1.9398        -0.41698
v  Velocity[z]            -43.216          58.428          0.5075        -0.36006
v  CourantNb           0.00048915          254.19          6.4444         0.63472
v  FourierNb           5.3306e-06         0.12438       0.0030237      0.00016341
v  total_pressure           99685      1.0164e+05      1.0151e+05      1.0157e+05
v  LocalTime                 0.01         0.21436        0.068131          0.1824


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00050756          254.22          6.4474         0.63488


 TIME FOR THE TIME STEP                8:        0.34338E+03

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


 INSTANT    0.900000000E+00   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391811069E+03
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 0.00000E+00
   Friction velocity        uet   :  0.41136E-03 0.51681E+00
   Friction velocity        uk    :  0.41136E-03 0.51681E+00
   Dimensionless distance   yplus :  0.33074E+01 0.71871E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.77447E+03     747   0.33981E+01   0.20258E+01 
c  VelocityX    0.83839E+04     165   0.41316E-01   0.45244E+00 
c  VelocityY    0.83839E+04     165   0.41316E-01   0.18731E+00 
c  VelocityZ    0.83839E+04     165   0.41316E-01   0.20052E+01 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime        4.39e-05                        690541


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1651.5          314.61          184.07          239.07
v  Velocity[x]            -39.197          34.305          1.6432         0.92827
v  Velocity[y]            -45.413          38.873         -1.8038         -0.4166
v  Velocity[z]            -55.039          44.871         0.50113        -0.38778
v  CourantNb            0.0004705          227.79          6.3839         0.66606
v  FourierNb           5.3306e-06         0.12438       0.0030352      0.00017251
v  total_pressure           99674      1.0164e+05      1.0151e+05      1.0156e+05
v  LocalTime                 0.01         0.23579         0.07083          0.1958


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00049075          227.82           6.387         0.66623


 TIME FOR THE TIME STEP                9:        0.18927E+03

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


 INSTANT    0.100000000E+01   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.391810736E+03
Smooth wall               5      159926         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4         372         0.000000000E+00
Free outlet               3          58         0.391810902E+03
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 0.00000E+00
   Friction velocity        uet   :  0.25333E-03 0.45061E+00
   Friction velocity        uk    :  0.25333E-03 0.45061E+00
   Dimensionless distance   yplus :  0.29685E+01 0.72071E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     159926
   Total number of wall faces                   :     159926
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration         10, Physical time    0.10000E+01


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

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

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

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


 Time for restart files:    0.26007E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13650E+04    2324   0.32355E+01   0.18364E+01 
c  VelocityX    0.89759E+04     170   0.42813E-01   0.49171E+00 
c  VelocityY    0.89759E+04     170   0.42813E-01   0.20658E+00 
c  VelocityZ    0.89759E+04     170   0.42813E-01   0.59235E+01 
---------------------------------------------------------------
  
  

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

   field         initial min     initial max  clips to min  clips to max
-  ---------  --------------  --------------  ------------  ------------
a  LocalTime      3.6366e-05                        690831


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1686.6          331.41          173.46          226.73
v  Velocity[x]            -36.764          38.436           1.763         0.93319
v  Velocity[y]            -45.669          38.367         -1.7384        -0.41358
v  Velocity[z]            -102.67          63.771         0.49749        -0.44322
v  CourantNb            0.0022556          274.98          6.3242         0.69937
v  FourierNb           5.3282e-06         0.12438       0.0030463      0.00018119
v  total_pressure           99638      1.0166e+05       1.015e+05      1.0155e+05
v  LocalTime                 0.01         0.25937        0.073454          0.2088


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022779          275.01          6.3272         0.69955


 TIME FOR THE TIME STEP               10:        0.38367E+03

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.95973E-02
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:           3968.480 s
  System CPU time:           51.808 s

  Elapsed time:            4021.240 s
  CPU / elapsed time          1.000

Memory use summary:

  Total memory used:                               2.269 GiB
  Theoretical instrumented dynamic memory:         1.239 GiB
