command: 
 /work/projects/Code_Saturne/5.0.9/code_saturne-5.0.9/libexec/code_saturne/cs_solver --param setup.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 5.0.9


  Copyright (C) 1998-2018 EDF S.A., France

  revision 5.0.9-9b87d1bcb
  build Fri 23 Nov 2018 06:05:43 PM CET
  MPI version 3.1 (MPICH 3.2)


  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 02 Apr 2019 02:34:40 PM CEST
  System:              Linux 3.10.0-514.el7.x86_64
  Machine:             c06s13.iter.org
  Processor:           model name	: Intel(R) Xeon(R) CPU E5-2680 v4 @ 2.40GHz
  Memory:              128514 MB
  User:                raja (Raj Amit EXT)
  Directory:           /scratch/raja/PROJECTS/TEST/Test/RESU/RUN1
  MPI ranks:           56 (appnum attribute: 0)
  OpenMP threads:      1
  Processors/node:     28
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    ParMETIS 4.0.3
    PT-SCOTCH 6.0.4

 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   =              6 (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
    -------------


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


 ** 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
 k                 0.1000E-07      1
 epsilon           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 =           1000 (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
 k                              0
 epsilon                        0
 TurbVisc                    -999
 total_pressure              -999
 Yplus                       -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              1 (Force exerted by the
                                     fluid on the boundary)
       ipstyp =              1 (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: EnSight Gold
      options: 
      time dependency: fixed mesh
      output: at calculation end

   1: name: BOUNDARY
      directory: postprocessing
      format: EnSight Gold
      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
 No "partition_input/domain_number_56" file available;

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

 Partitioning 22311 cells to 56 domains on 56 ranks
   (SCOTCH_dgraphPart).

  wall-clock time: 0.273241 s

  Number of cells per domain (histogramm):
    [        369 ;        374 [ =          1
    [        374 ;        379 [ =          3
    [        379 ;        384 [ =          6
    [        384 ;        389 [ =          6
    [        389 ;        394 [ =          4
    [        394 ;        399 [ =          2
    [        399 ;        404 [ =         11
    [        404 ;        409 [ =          8
    [        409 ;        414 [ =          5
    [        414 ;        419 ] =         10

 Writing file:        partition_output/domain_number_56
 Finished writing:    partition_output/domain_number_56

 Partitioning finished (0.611 s)


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

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

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

 Histogram of the number of cells per rank:

    minimum value =                369
    maximum value =                419

      1 : [        369 ;        379 [ =          4
      2 : [        379 ;        389 [ =         12
      3 : [        389 ;        399 [ =          6
      4 : [        399 ;        409 [ =         19
      5 : [        409 ;        419 ] =         15

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

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

    minimum value =                571
    maximum value =                745

      1 : [        571 ;        605 [ =          3
      2 : [        605 ;        640 [ =         11
      3 : [        640 ;        675 [ =         16
      4 : [        675 ;        710 [ =         20
      5 : [        710 ;        745 ] =          6

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

 Histogram of the number of ghost cells per rank:

    minimum value =                191
    maximum value =                337

      1 : [        191 ;        220 [ =          9
      2 : [        220 ;        249 [ =          3
      3 : [        249 ;        278 [ =         22
      4 : [        278 ;        307 [ =         17
      5 : [        307 ;        337 ] =          5

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

 Histogram of the number of interior faces per rank:

    minimum value =               1172
    maximum value =               1417

      1 : [       1172 ;       1221 [ =          3
      2 : [       1221 ;       1270 [ =         11
      3 : [       1270 ;       1319 [ =         16
      4 : [       1319 ;       1368 [ =         15
      5 : [       1368 ;       1417 ] =         11

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

 Histogram of the number of boundary faces per rank:

    minimum value =                  0
    maximum value =                140

      1 : [          0 ;         28 [ =          8
      2 : [         28 ;         56 [ =         30
      3 : [         56 ;         84 [ =          7
      4 : [         84 ;        112 [ =          6
      5 : [        112 ;        140 ] =          5

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

 Histogram of the number of interior faces per cell:

    minimum value =                  4
    maximum value =                  6

      1 : [          4 ;          5 [ =         72
      2 : [          5 ;          6 ] =      22239

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  5
    maximum value =                 17

      1 : [          5 ;          7 [ =         10
      2 : [          7 ;          9 [ =         21
      3 : [          9 ;         12 [ =         17
      4 : [         12 ;         14 [ =          5
      5 : [         14 ;         17 ] =          3

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

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

 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =                472
    maximum value =                703

      1 : [        472 ;        518 [ =          4
      2 : [        518 ;        564 [ =         11
      3 : [        564 ;        610 [ =         19
      4 : [        610 ;        656 [ =         18
      5 : [        656 ;        703 ] =          4

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =                172
    maximum value =                286

      1 : [        172 ;        194 [ =          3
      2 : [        194 ;        217 [ =          7
      3 : [        217 ;        240 [ =         21
      4 : [        240 ;        263 [ =         20
      5 : [        263 ;        286 ] =          5

 Mesh coordinates:               minimum    and maximum
                       X : -1.0957398e-02  1.1000000e-01
                       Y : -1.2095740e-01  0.0000000e+00
                       Z : -1.0996995e-02  1.0996995e-02
 Mesh
     Number of cells:          22311
     Number of interior faces: 65394
     Number of boundary faces: 3078
     Number of vertices:       23936

 Groups:
    "INLET"
       boundary faces:          333
    "OUTLET"
       boundary faces:          333
    "WALL"
       boundary faces:         2412

 --- Information on the volumes
       Minimum control volume      =  2.9754561e-10
       Maximum control volume      =  6.3485894e-09
       Total volume for the domain =  7.9608739e-05

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

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 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 (0.00185 s)
                                                             
       ALMAX  =    0.43018E-01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  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
  k                 0.6000E-03  0.6000E-03
  epsilon           0.3075E-04  0.3075E-04
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E+01   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.1242E-02  0.1242E-02
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         333
Smooth wall               5        2412
Rough wall                6           0
Symmetry                  4           0
Free outlet               3         333
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 =    0.11000E+00  -0.99413E-01  -0.40281E-08



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         333         0.000000000E+00
Smooth wall               5        2412         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         333         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    :  0.23735E-02 0.33400E-02
   Dimensionless distance   yplus :  0.33890E-01 0.95966E-01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2412
   Total number of wall faces                   :       2412
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          1
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


 Wall-clock time limit set by CS_MAXTIME: 299h:59m:56s

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.14645E-04      49   0.15801E-01   0.57689E+04 0.57790E+04 
c  Velocity[X]                                      0.29078E+04 
c  Velocity[Y]                                      0.28575E+04 
c  Velocity[Z]                                      0.35886E+01 
c  Pressure     0.23941E-04      29   0.26707E+00   0.99997E+00 0.70601E+04 
c  k            0.10662E-05      44   0.21046E-02   0.21534E-03 0.19214E+04 
c  epsilon      0.12113E-06      49   0.42998E-02   0.35099E-04 0.54072E+04 
----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.19256          1.8259         0.47318         0.51257
v  Velocity[Y]            -1.8755       0.0022021          -0.481        -0.50422
v  Velocity[Z]           -0.19161         0.19161      2.2087e-08      1.2452e-08
v  ǁVelocityǁ             0.12741          2.1242         0.88615         0.97104
v  Pressure                3.7626          437.75          220.86          220.27
v  k                   0.00029619       0.0025096      0.00056936      0.00056832
v  epsilon             3.0745e-05      0.00081395       4.071e-05      4.2945e-05
v  TurbVisc             0.0012419       0.0012419       0.0012419       0.0012419
v  total_pressure      1.0133e+05      1.0176e+05      1.0155e+05      1.0155e+05

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

   field         minimum         maximum        set mean    spatial mean
