command: 
 /home/lgarelli/Code_Saturne_5/libexec/code_saturne/cs_solver --param setup.xml

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

                                  (R)
                      Code_Saturne

                      Version 5.0.0


  Copyright (C) 1998-2017 EDF S.A., France

  revision 5.0.0
  build Fri 09 Jun 2017 03:52:35 PM ART
  MPI version 3.0 (MPICH 3.1)


  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:                Tue 24 Oct 2017 12:10:18 PM ART
  System:              Linux 4.0.6-200.fc21.x86_64 (Fedora release 21 (Twenty One))
  Machine:             localhost.localdomain
  Processor:           model name	: Intel(R) Core(TM) i7 CPU       Q 720  @ 1.60GHz
  Memory:              7903 MB
  User:                lgarelli (lgarelli)
  Directory:           /home/lgarelli/RUNS/Code_Saturne/Tang_vel_test/RESU/Test
  OpenMP threads:      1
  Processors/node:     8
  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"

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

                   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 )


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


 ** VOF METHOD                              
    ----------------------------------------

       IVOFMT =             -1 ( -1: inactive                )
                               (  0: active                  )


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

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


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


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

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  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      )
                                                             

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


 ** STOKES
    ------

  -- Phase continue :

       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                   )


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
------------------------------------

       EPSILO =                (resolution precision)
       IDIRCL = 0 ou 1         (shift diagonal if
                                ISTAT=0 and no Dirichlet)


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


 ** 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 )

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
         --           --                --

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

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

 Velocity                       0
 Pressure                       0
 CourantNb                   -999
 FourierNb                   -999
 total_pressure              -999
         --           --                --

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


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


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

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


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


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

  -1: name: results
      directory: postprocessing
      format: MED 3.2.1
      options: 
      time dependency: fixed mesh
      output: at calculation end

  -5: name: 
      directory: monitoring
      format: time_plot
      options: 
      time dependency: fixed mesh
      output: every 1 time steps

  -6: name: 
      directory: profiles
      format: plot
      options: 
      time dependency: fixed mesh
      output: at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input

 Extended neighborhood structures definition
 Number of cells:                                      10000

 ----------------------------------------------------------
 Number of cells + halo cells:                         10000


 ----------------------------------------------------------
 Number of interior faces:                             29100

 ----------------------------------------------------------
 Number of boundary faces:                             1800

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

 Histogram of the number of interior faces per cell:

    minimum value =                  4
    maximum value =                  6

      1 : [          4 ;          5 [ =         80
      2 : [          5 ;          6 ] =       9920

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

 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

 Matrix bandwidth for volume mesh :          8000
 Matrix profile/lines for volume mesh :      1270

 Mesh coordinates:               minimum    and maximum
                       X : -1.0000000e+00  1.0000000e+00
                       Y : -1.0000000e+00  1.0000000e+00
                       Z :  0.0000000e+00  1.0000000e+01
 Mesh
     Number of cells:          10000
     Number of interior faces: 29100
     Number of boundary faces: 1800
     Number of vertices:       10941

 Groups:
    "inlet"
       boundary faces:          400
    "outlet"
       boundary faces:          500
    "wall"
       interior faces:         2100
       boundary faces:          900

 --- Information on the volumes
       Minimum control volume      =  2.8413783e-04
       Maximum control volume      =  8.0802000e-03
       Total volume for the domain =  3.1286893e+01

  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: 0 -->   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 %

 Computing geometric quantities (0.0262 s)
                                                             
       ALMAX  =    0.31510E+01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.


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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
 ---------------------------------

                dt  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
  molecular_viscos  0.1000E+00  0.1000E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         400
Smooth wall               5         900
Rough wall                6           0
Symmetry                  4           0
Free outlet               3         500
Free inlet               14           0
Convective inlet         16           0
Free surface             15           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =   -0.67000E-01   0.27171E-16   0.10000E+02



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.000000000E+00
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.14419E+01     157   0.35202E-02   0.79513E-01 0.10000E+02 
c  Velocity[X]                                      0.39756E-01 
c  Velocity[Y]                                      0.39756E-01 
c  Velocity[Z]                                      0.48736E-07 
c  Pressure     0.10716E-02      18   0.45296E-02   0.34181E+00 0.10000E+02 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.81815         0.81815      1.7408e-13      1.1057e-13
v  Velocity[Y]           -0.81815         0.81815     -9.0816e-13      -9.606e-14
v  Velocity[Z]         -0.0013424       0.0013424     -3.0234e-12     -3.9637e-12
v  ǁVelocityǁ          5.0553e-13         0.82057        0.079197         0.01626
v  Pressure             -0.008283        0.008283     -6.4584e-10     -4.6918e-10
v  CourantNb                    0               0               0               0
v  FourierNb               3.7906          21.017          9.3169          7.7502
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.7906          21.017          9.3169          7.7502


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.283942539E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.19397E-05 0.11006E+01
   Friction velocity        uk    :  0.19397E-05 0.11006E+01
   Dimensionless distance   yplus :  0.41841E-06 0.64862E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15668E+01     154   0.29904E-02   0.95400E-02 0.26896E+01 
c  Velocity[X]                                      0.47698E-02 
c  Velocity[Y]                                      0.47698E-02 
c  Velocity[Z]                                      0.51551E-06 
c  Pressure     0.43488E-02      20   0.53364E-02   0.76620E+00 0.10000E+02 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.90741         0.90741     -1.7481e-12     -1.9847e-12
v  Velocity[Y]           -0.90741         0.90741      1.8579e-12     -2.5543e-13
v  Velocity[Z]         -0.0040248       0.0027259      4.2488e-06     -2.9904e-06
v  ǁVelocityǁ          3.2242e-12         0.91031         0.11808        0.023827
v  Pressure             -0.010942        0.025571      -1.319e-05     -2.7154e-07
v  CourantNb           8.3037e-13         0.60379        0.073327        0.014306
v  FourierNb               3.8011          22.484          9.4879          7.7877
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.8011          23.088          9.5612           7.802


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.929254698E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.45162E-05 0.11429E+01
   Friction velocity        uk    :  0.45162E-05 0.11429E+01
   Dimensionless distance   yplus :  0.10768E-05 0.67354E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15875E+01     151   0.20026E-02   0.35639E-02 0.14675E+01 
c  Velocity[X]                                      0.17817E-02 
c  Velocity[Y]                                      0.17817E-02 
c  Velocity[Z]                                      0.47005E-06 
c  Pressure     0.43060E-02      19   0.32849E-02   0.45557E+00 0.55258E+01 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.93113         0.93113     -5.4818e-12     -4.1783e-12
v  Velocity[Y]           -0.93113         0.93113      4.1386e-12     -3.4178e-13
v  Velocity[Z]         -0.0050849       0.0044746       1.343e-05     -7.3233e-06
v  ǁVelocityǁ          1.6499e-13         0.93418          0.1443        0.028852
v  Pressure             -0.017188         0.05446       0.0013439      0.00030754
v  CourantNb           2.1001e-12         0.66434         0.11892        0.022469
v  FourierNb               3.8011          22.484          9.4879          7.7877
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.8011          23.149          9.6068          7.8101


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.624465417E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.77532E-06 0.11496E+01
   Friction velocity        uk    :  0.77532E-06 0.11496E+01
   Dimensionless distance   yplus :  0.21058E-06 0.67746E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15946E+01     149   0.15219E-02   0.18388E-02 0.98273E+00 
c  Velocity[X]                                      0.91919E-03 
c  Velocity[Y]                                      0.91919E-03 
c  Velocity[Z]                                      0.41471E-06 
c  Pressure     0.35381E-02      19   0.24706E-02   0.27911E+00 0.35387E+01 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.94274         0.94274     -7.6656e-12     -5.5492e-12
v  Velocity[Y]           -0.94274         0.94274      5.4726e-12     -4.5511e-13
v  Velocity[Z]         -0.0052948       0.0059236      2.3457e-05     -1.2321e-05
v  ǁVelocityǁ          7.4763e-14         0.94588         0.16393         0.03264
v  Pressure             -0.020869        0.081102       0.0032349       0.0007293
v  CourantNb           2.4711e-13         0.72567         0.15243        0.028412
v  FourierNb               3.7967          22.484          9.4878          7.7875
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.7967          23.163          9.6402          7.8159


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.624628339E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.54048E-06 0.11518E+01
   Friction velocity        uk    :  0.54048E-06 0.11518E+01
   Dimensionless distance   yplus :  0.13127E-06 0.67874E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15985E+01     146   0.16348E-02   0.10929E-02 0.72121E+00 
c  Velocity[X]                                      0.54627E-03 
c  Velocity[Y]                                      0.54627E-03 
c  Velocity[Z]                                      0.40112E-06 
c  Pressure     0.27315E-02      19   0.19807E-02   0.17975E+00 0.24403E+01 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.94968         0.94968     -7.4763e-12        -5.8e-12
v  Velocity[Y]           -0.94968         0.94968      4.8939e-12     -6.6402e-13
v  Velocity[Z]         -0.0056558       0.0069446      3.3681e-05      -1.634e-05
v  ǁVelocityǁ          3.0896e-12          0.9529         0.17931        0.035662
v  Pressure             -0.025073         0.10534        0.005158       0.0011513
v  CourantNb           1.5408e-13         0.80136         0.17869        0.033118
v  FourierNb               3.8011          22.484          9.4878          7.7876
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.8011           23.17          9.6665          7.8207


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.797151170E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.32826E-05 0.11530E+01
   Friction velocity        uk    :  0.32826E-05 0.11530E+01
   Dimensionless distance   yplus :  0.80056E-06 0.67948E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16012E+01     144   0.12971E-02   0.70122E-03 0.55669E+00 
c  Velocity[X]                                      0.35041E-03 
c  Velocity[Y]                                      0.35041E-03 
c  Velocity[Z]                                      0.40595E-06 
c  Pressure     0.20332E-02      19   0.18291E-02   0.11915E+00 0.17695E+01 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.95452         0.95452      -8.374e-12     -6.3824e-12
v  Velocity[Y]           -0.95452         0.95452      5.9263e-12     -3.9446e-13
v  Velocity[Z]         -0.0060787       0.0078878      3.7797e-05     -1.9871e-05
v  ǁVelocityǁ          3.3715e-13         0.95779         0.19165        0.038145
v  Pressure             -0.029655         0.12627       0.0069293       0.0015242
v  CourantNb           6.9261e-13          0.8877         0.19977        0.036979
v  FourierNb               3.8011          22.484          9.4879          7.7877
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.8011          23.174          9.6876          7.8247


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.217003812E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.66240E-05 0.11537E+01
   Friction velocity        uk    :  0.66240E-05 0.11537E+01
   Dimensionless distance   yplus :  0.16821E-05 0.67991E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16033E+01     142   0.13903E-02   0.47139E-03 0.44343E+00 
c  Velocity[X]                                      0.23549E-03 
c  Velocity[Y]                                      0.23549E-03 
c  Velocity[Z]                                      0.41164E-06 
c  Pressure     0.15346E-02      18   0.15934E-02   0.83153E-01 0.13656E+01 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.95799         0.95799     -7.7808e-12     -6.3483e-12
v  Velocity[Y]           -0.95799         0.95799      4.6213e-12     -6.4437e-13
v  Velocity[Z]         -0.0077925       0.0087314      4.2905e-05     -2.2605e-05
v  ǁVelocityǁ          5.0199e-13         0.96131         0.20171        0.040222
v  Pressure             -0.034983         0.14373       0.0085318        0.001852
v  CourantNb           9.0406e-13          1.0241         0.21695        0.040212
v  FourierNb               3.7967          22.484          9.4876          7.7871
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.7967          23.177          9.7045          7.8273


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.575956211E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.23726E-05 0.11549E+01
   Friction velocity        uk    :  0.23726E-05 0.11549E+01
   Dimensionless distance   yplus :  0.71755E-06 0.68059E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16049E+01     140   0.13533E-02   0.32658E-03 0.36064E+00 
c  Velocity[X]                                      0.16310E-03 
c  Velocity[Y]                                      0.16310E-03 
c  Velocity[Z]                                      0.38306E-06 
c  Pressure     0.11552E-02      18   0.14054E-02   0.59326E-01 0.10481E+01 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.96062         0.96062     -8.2485e-12      -6.521e-12
v  Velocity[Y]           -0.96062         0.96062      5.6438e-12     -2.5132e-13
v  Velocity[Z]         -0.0095696       0.0096284      4.3577e-05     -2.5611e-05
v  ǁVelocityǁ          1.1747e-12         0.96357         0.21001        0.041981
v  Pressure             -0.039948         0.15858       0.0099706       0.0021377
v  CourantNb            1.148e-12          1.1483         0.23111        0.042951
v  FourierNb               3.8011          22.484          9.4879          7.7877
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.8011          23.179           9.719          7.8306


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.136136011E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.66314E-05 0.11546E+01
   Friction velocity        uk    :  0.66314E-05 0.11546E+01
   Dimensionless distance   yplus :  0.16588E-05 0.68040E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16062E+01     138   0.13161E-02   0.23057E-03 0.29736E+00 
c  Velocity[X]                                      0.11509E-03 
c  Velocity[Y]                                      0.11509E-03 
c  Velocity[Z]                                      0.37703E-06 
c  Pressure     0.88531E-03      18   0.13011E-02   0.43815E-01 0.86462E+00 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.9627          0.9627     -4.1939e-11      -1.634e-11
v  Velocity[Y]            -0.9627          0.9627      3.0633e-11      4.0034e-12
v  Velocity[Z]          -0.011397        0.010533       4.458e-05     -2.8275e-05
v  ǁVelocityǁ          2.0161e-13         0.96609         0.21691        0.043481
v  Pressure              -0.04549         0.17158         0.01128       0.0023938
v  CourantNb           1.2586e-12          1.2518          0.2429        0.045295
v  FourierNb               3.7967          22.484          9.4875           7.787
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.7967           23.18          9.7304          7.8323


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         400         0.142681006E-15
Smooth wall               5         900         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         500        -0.273700565E-10
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           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   :  0.77606E-06 0.11548E+01
   Friction velocity        uk    :  0.77606E-06 0.11548E+01
   Dimensionless distance   yplus :  0.22655E-06 0.68054E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        900
   Total number of wall faces                   :        900
------------------------------------------------------------




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


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

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

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

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

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16073E+01     136   0.12746E-02   0.16485E-03 0.24755E+00 
c  Velocity[X]                                      0.82256E-04 
c  Velocity[Y]                                      0.82256E-04 
c  Velocity[Z]                                      0.33868E-06 
c  Pressure     0.70836E-03      18   0.10949E-02   0.34105E-01 0.70290E+00 
----------------------------------------------------------------------------
  
  

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.96388         0.96388     -4.5394e-11     -1.9797e-11
v  Velocity[Y]           -0.96388         0.96388       2.925e-11      2.3079e-12
v  Velocity[Z]          -0.013205         0.01125      4.2729e-05     -3.0217e-05
v  ǁVelocityǁ            1.45e-12          0.9673         0.22269        0.044767
v  Pressure             -0.051057         0.18192        0.012425       0.0026188
v  CourantNb           6.6939e-13          1.3401         0.25277        0.047312
v  FourierNb               3.8011          22.484          9.4878          7.7876
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.8011          23.182          9.7406          7.8349



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



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


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





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




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


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

 Destroying structures and ending computation
