command: 
 ./cs_solver --param test_LES_2.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.3.2


  Copyright (C) 1998-2014 EDF S.A., France

  build Mon 15 Dec 2014 07:37:43 PM GMT
  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 16 Dec 2014 10:36:30 AM GMT
  System:              Linux 3.0.80-0.5.1_1.0501.7664-cray_ari_c
  Machine:             nid02313
  Processor:           model name	: Intel(R) Xeon(R) CPU E5-2697 v2 @ 2.70GHz
  Memory:              64517 MB
  Directory:           /fs3/e01/e01/qmul01/test_2/CASE1/RESU/20141216-1036
  MPI ranks:           1 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)

  External libraries for partitioning:
    ParMETIS 4.0.2
    PT-SCOTCH 6.0.0

 Reading metadata from file: "mesh_input"

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

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


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



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

@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@
@ @@   WARNING :      WHILE READING INPUT DATA
@    =========
@    RISQUE DE PERTE D'INFORMATION EN CALCUL SUITE
@
@  The calculation will run.
@
@ A turbulence model was activated by ITURB =         42
@    but writing to auxiliary restart file was de-activated
@
@    ILEAUX =          0    IECAUX =          1
@  Although this file is not necessary to restart
@  a computation, it does contain information that avoid
@   numerical perturbations when restarting a computation
@
@
@ Check the input data given through the User Interface
@   or in cs_user_parameters.f90.
@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@


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


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

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

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


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

 --- Physics
       NVAR   =              4 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              9 (Nb cell properties          )


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


 ** 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

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


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

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


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


 ** 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  =             42 (Turbulence model            )
       IDEUCH =              0 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.10880E+02 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

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

   - Commons
       XKAPPA =    0.42000E+00 (Von Karman constant         )
       CSTLOG =    0.52000E+01 (U+=Log(y+)/kappa +CSTLOG    )
       APOW   =    0.83000E+01 (U+=APOW (y+)**BPOW (W&W law))
       BPOW   =    0.14286E+00 (U+=APOW (y+)**BPOW (W&W law))


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


 ** SECONDARY VISCOSITY
    -------------------

 --- Continuous phase:
       IVISSE =              1 (1: accounted for            )


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.10000E-07 (Minimum time step           )
       DTMAX  =    0.10000E-03 (Maximum time step           )
       DTREF  =    0.10000E-06 (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
------------------------------------
 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 =              2 (1: order 1; 2: order 2      )
                                                             

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


 ** CONVECTION - DIFFUSION
    ----------------------

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Velocity              1      1      1      1      1 0.10E+01 0.50E+00
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
-------------------------------------------------------------

       ICONV  =  0 ou  1       (1 for convection active     )
       IDIFF  =  0 ou  1       (1 for total diffusion active)
       IDIFFT =  0 ou  1       (1 for turbulent diff. active)
       ISCHCV =  0 ou  1       (SOLU or CD                  )
       ISSTPC =  0 ou  1       (1: no slope test            )
       BLENCV =  [0.;1.]       (1-upwind proportion         )
       THETAV =  [0.;1.]       (0.5 Crank-Nicolson/AB       )
                               (theta for convection-       )
                               (diffusion terms uses        )
                               ((1-theta).old+theta.new     )


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


 ** STOKES
    ------
       IDILAT =              1 (1 : without unsteady term
                                    in the continuity equation
                                2 : with unsteady term in 
                                    the continuity equation)
       IPOROS =              0 (0 : without porous media
                                1 : with porous media)
       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 =              2 (time scheme for flow
                               (0: explicit (THETFL = 0     )
                               (1: std scheme (Saturne 1.0  )
                               (2: 2nd-order (THETFL = 0.5  )
       THETFL =    0.50000E+00 (theta for mass flow         )
       IROEXT =              0 (density extrapolation
                               (0: explicit
                               (1: n+thetro with thetro=1/2
                               (2: n+thetro with thetro=1
       THETRO =    0.00000E+00 (theta for density
                               ((1+theta).new-theta.old
       IVIEXT =              0 (total viscosity extrapolation
                               (0: explicit
                               (1: n+thetvi with thetro=1/2
                               (2: n+thetvi with thetro=1
       THETVI =    0.00000E+00 (theta for total viscosity
                               ((1+theta).new-theta.old
       ICPEXT =              0 (specific heat extrapolation
                               (0: explicit
                               (1: n+thetcp with thetro=1/2
                               (2: n+thetcp with thetro=1
       THETCP =    0.00000E+00 (specific heat theta-scheme
                               ((1+theta).new-theta.old
       THETSN =    0.50000E+00 (Nav-Stokes S.T. theta scheme)
                               ((1+theta).new-theta.old
       THETST =    0.00000E+00 (Turbulence S.T. theta-scheme)
                               ((1+theta).new-theta.old
       EPSUP  =    0.10000E-04 (Velocity/pressure coupling
                                stop test                   )


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


 ** GRADIENTS CALCULATION
    ---------------------

       IMRGRA =              0 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100     10  0.1000E-04  0.1000E-03  0.0000E+00
 Pressure            100      5  0.1000E-04  0.1000E-03  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              1     -1  0.1500E+01
 Pressure              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                )


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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Velocity             -1  10000  0.1000E-04      1
 Pressure              0  10000  0.1000E-04      1
-----------------------------------

       IRESOL =            -1  (automatic solver choice     )
                IPOL*1000 + 0  (p conjuguate gradient       )
                            1  (Jacobi                      )
                IPOL*1000 + 2  (bicgstab                    )
                  avec IPOL    (preconditioning degree      )
       NITMAX =                (max number of iterations    )
       EPSILO =                (resolution precision        )
       IDIRCL = 0 ou 1         (shift diagonal if   
                                ISTAT=0 and no Dirichlet    )


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


 ** MULTIGRID
    ---------

       NCEGRM =             30 (Max nb cells coarsest grid  )
       NGRMAX =             25 (Max number of levels        )
--------------------------------------
 Variable           IMGR NCYMAX NITMGF
--------------------------------------                       
 Velocity              0    100     10
 Pressure              1    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 =              0 (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 =            150 (Final time step required    )

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


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


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

 --- Restart file
       NTSUIT =            100 (Checkpoint frequency )

 --- Post-processed variables

       Number Name
Velocity
Pressure
CourantNb
FourierNb
total_pressure
navier_stokes_st_prev[
         --           --

 --- 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 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 Density                       -1
         7 LamVisc                       -1
         9 CourantNb                     -1
        10 FourierNb                     -1
        11 total_pressure                -1
        12 navier_stokes_st              -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         9 CourantNb                   -999
        10 FourierNb                   -999
        11 total_pressure              -999
        12 navier_stokes_st            -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: CGNS 3.2.1

      options: 
      time dependency: fixed mesh
      output: every 50 time steps and at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input


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

  Periodicity type: translation
  Transformation matrix:             1            0            0            0
                                     0            1            0            0
                                     0            0            1        0.004

  Selection criteria: "SIDE_1 or SIDE_2"

  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:          4312768
     Number of interior faces: 12840420
     Number of boundary faces: 195768
     Number of vertices:       4411200

  Global number of boundary faces selected for joining:     109184

  Element selection successfully done.
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       879300
    Vertex-Vertex intersections:          879300
    Other intersections:                       0

  Joining operation is conforming.

  Edge intersections and vertex creation done.

  Pre-merge for 55140 global element couples.

  No need to merge vertices.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:     163776

  Global configuration after the joining operation:
     Global number of border faces to add:          0

  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:          4312768
     Number of interior faces: 12949604
     Number of boundary faces: 86584
     Number of vertices:       4411200


  Joining  1 completed (12.8 s).

  All joining operations successfully finished:

    Wall clock time:                  15.5


 ----------------------------------------------------------
 Composing periodicities

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

 Face interfaces creation
 Definition of periodic vertices
 Vertex interfaces creation
 Halo creation
 Halo definition
    Local halo definition
    Distant halo creation
    Updating the faces -> cells connectivity
 Number of cells:                                      4312768

 ----------------------------------------------------------
 Number of cells + halo cells:                         4421952


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

 Number of ghost cells:                              109184

 ----------------------------------------------------------
 Number of interior faces:                             12949604

 ----------------------------------------------------------
 Number of boundary faces:                             86584

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

 Histogram of the number of interior faces per cell:

    minimum value =                  4
    maximum value =                  6

      1 : [          4 ;          5 [ =        316
      2 : [          5 ;          6 ] =    4312452

 ----------------------------------------------------------
Synchronizing cell families

 Writing file:        mesh_output
 Finished writing:    mesh_output

 ----------------------------------------------------------
 Composing periodicities

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

 Face interfaces creation
 Definition of periodic vertices
 Vertex interfaces creation
 Halo creation
 Halo definition
    Local halo definition
    Distant halo creation
    Updating the faces -> cells connectivity
 Number of cells:                                      4312768

 ----------------------------------------------------------
 Number of cells + halo cells:                         4421952


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

 Number of ghost cells:                              109184

 ----------------------------------------------------------
 Number of interior faces:                             12949604

 ----------------------------------------------------------
 Number of boundary faces:                             86584

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

 Histogram of the number of interior faces per cell:

    minimum value =                  4
    maximum value =                  6

      1 : [          4 ;          5 [ =        316
      2 : [          5 ;          6 ] =    4312452

 ----------------------------------------------------------
Synchronizing cell families

 Renumbering mesh:

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


 Matrix bandwidth for volume mesh :          4367360
 Matrix profile/lines for volume mesh :      93914

 Mesh coordinates:               minimum    and maximum
                       X : -2.0000000e-02  5.0000001e-02
                       Y : -2.0000000e-02  2.0000000e-02
                       Z : -2.0000000e-03  2.0000000e-03
 Mesh
     Number of cells:          4312768
     Number of interior faces: 12949604
     Number of boundary faces: 86584
     Number of vertices:       4411200

 Periodic faces (which are also interior faces):
     Periodicity  1:          54592 face couples

 Groups:
    "BOTTOM"
       boundary faces:        24727
    "INLET"
       boundary faces:        10823
    "OUTLET"
       boundary faces:        10823
    "SIDE_1"
       interior faces:        54592
    "SIDE_2"
       interior faces:        54592
    "TOP"
       boundary faces:        24727
    "WALL"
       boundary faces:        15484

 --- Information on the volumes
       Minimum control volume      =  2.0330388e-15
       Maximum control volume      =  4.8663263e-11
       Total volume for the domain =  1.1196856e-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 (5.93 s)
                                                             
       ALMAX  =    0.22457E-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-06  0.1000E-06
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-06   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  0.0000E+00  0.0000E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2       10823
Smooth wall               5       15484
Rough wall                6           0
Symmetry                  4       49454
Free outlet               3       10823
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.50000E-01   0.93434E-10  -0.44819E-17



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       10823         0.000000000E+00
Smooth wall               5       15484         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       49454         0.000000000E+00
Free outlet               3       10823         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     :      15484
   Total number of wall faces                   :      15484
------------------------------------------------------------


   0.0000000000000000        0.0000000000000000        0.0000000000000000     

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.46715E-05       3   0.23754E-06   0.32336E-01 
c  VelocityY    0.46715E-05       3   0.23754E-06   0.00000E+00 
c  VelocityZ    0.46715E-05       3   0.23754E-06   0.00000E+00 
c  Pressure     0.15610E-03    2203   0.15059E-02   0.10000E+01 
---------------------------------------------------------------
  
  

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

   field                          minimum         maximum        set mean    spatial mean
-  ----------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                    0.30797          113.88          56.928          56.587
v  Velocity[Y]                     -56.58           56.58       9.956e-06      8.1546e-07
v  Velocity[Z]                   -0.11078         0.11142      1.0505e-10      4.1083e-13
v  ǁVelocityǁ                     0.30805          113.88          58.328          56.592
v  Pressure                         79797      4.6707e+07       2.508e+07      2.3518e+07
v  CourantNb                            0               0               0               0
v  FourierNb                    0.0012145         0.47368         0.02648       0.0015024
v  total_pressure              1.8112e+05      4.6808e+07      2.5181e+07      2.3619e+07
v  navier_stokes_st_prev[               0               0               0               0
v  navier_stokes_st_prev[               0               0               0               0
v  navier_stokes_st_prev[               0               0               0               0


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012145         0.47368         0.02648       0.0015024


 TIME FOR THE TIME STEP                1:        0.27099E+03

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


 INSTANT    0.200000000E-06   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       10823        -0.143320189E-01
Smooth wall               5       15484         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       49454         0.000000000E+00
Free outlet               3       10823         0.143318529E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29264E+00 0.37573E+02
   Friction velocity        uk    :  0.29264E+00 0.37573E+02
   Dimensionless distance   yplus :  0.23606E-01 0.30308E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      15484
   Total number of wall faces                   :      15484
------------------------------------------------------------


   1.1046217656913682E-002   3.3330733324915016E-009   2.8345960098599107E-013
===========================================================
   ** Stop to avoid exceeding time allocation.
      ----------------------------------------
      maximum time step number set to: 2
===========================================================
===============================================================
   ** Remaining time management
      -------------------------
      Remaining time allocated to the job       : ',    1.87487e+02
      Estimated time for another time step      : ',    3.95701e+02
        mean time for a time step               : ',    4.12513e+02
        time for the previous time step         : ',    1.05268e+02
        security margin                         : ',    6.00000e+01
===============================================================


 Write final restart files
   checkpoint at iteration          2, Physical time    0.20000E-06


   ** 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 the source terms                         
 End writing


 Time for restart files:    0.22406E+01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.80712E+01       2   0.52382E-05   0.16151E-02 
c  VelocityY    0.80712E+01       2   0.52382E-05   0.00000E+00 
c  VelocityZ    0.80712E+01       2   0.52382E-05   0.00000E+00 
c  Pressure     0.55090E-04     657   0.98027E-04   0.10000E+01 
---------------------------------------------------------------
  
  

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

   field                          minimum         maximum        set mean    spatial mean
-  ----------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                    0.20317          113.13          56.917          56.803
v  Velocity[Y]                    -55.373           55.34     -1.2088e-05     -2.7771e-07
v  Velocity[Z]                   -0.11095         0.11093      2.1526e-11      6.7185e-14
v  ǁVelocityǁ                     0.20324          113.13          58.313          56.807
v  Pressure                       -6818.2      1.7979e+05          499.98          2914.5
v  CourantNb                    0.0072236         0.94521         0.17793        0.034663
v  FourierNb                    0.0012194           7.077        0.052812       0.0019444
v  total_pressure                   94507      2.8111e+05      1.0182e+05      1.0424e+05
v  navier_stokes_st_prev[               0               0               0               0
v  navier_stokes_st_prev[               0               0               0               0
v  navier_stokes_st_prev[               0               0               0               0


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0084457          7.8229         0.23074        0.036608


 TIME FOR THE TIME STEP                2:        0.10999E+03

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.18504E+00
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:            364.963 s
  System CPU time:           38.378 s

  Elapsed time:             418.065 s
  CPU / elapsed time          0.965

Memory use summary:

  Total memory used:                               7.162 GiB
  Theoretical instrumented dynamic memory:         4.645 GiB
