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

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

                                  (R)
                      Code_Saturne

                      Version 3.0.0


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

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


  The Code_Saturne CFD tool  is free software;
  you can redistribute it and/or modify it under the terms
  of the GNU General Public License as published by the
  Free Software Foundation; either version 2 of the License,
  or (at your option) any later version.

  The Code_Saturne CFD tool is distributed in the hope that
  it will be useful, but WITHOUT ANY WARRANTY; without even
  the implied warranty of MERCHANTABILITY or FITNESS FOR A
  PARTICULAR PURPOSE.  See the GNU General Public License
  for more details.

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


Local case configuration:

  Date:                Wed 18 Nov 2015 12:46:13 AM CET
  System:              Linux 3.2.0-60-generic
  Machine:             caelinux
  Processor:           model name	: Intel(R) Core(TM) i5 CPU       M 560  @ 2.67GHz
  Memory:              3755 MB
  User:                caelinux (Live session user)
  Directory:           /home/caelinux/OUTLET-ONLY4/HIGH/RESU/20151118-0046
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

  External libraries for partitioning:
    ParMETIS 3.1
    PT-SCOTCH 1.12.2147483631

 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
    ----------

 --- Geometry
       NPRFML =              1 (Nb max. family properties   )
       NFML   =              4 (Nb families                 )

 --- Physics
       NVAR   =              4 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )
       NPROFA =              1 (Nb internal face properties )
       NPROFB =              2 (Nb boundary face properties )


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


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

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

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

  -- Continuous phase:

       RO0    =    0.72000E+03 (Reference density           )
       VISCL0 =    0.48000E-03 (Ref. molecular dyn. visc.   )
       CP0    =    0.22200E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =              0 (Turbulence model            )
       IDEUCH =              0 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )
       ISCALT =             -1 (Temperature salar number    )

 --- Constants

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


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

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

       With a non-constant time step (IDTVAR = 1 or 2),
         when the value of COUMAX or FOUMAX is negative
         or zero, the associated time step limitation (for
         CFL and Fourier respectively) is ignored.

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Pressure              0  0.1000E+01
 VelocityX             1  0.1000E+01
 VelocityY             1  0.1000E+01
 VelocityZ             1  0.1000E+01
----------------------------

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

 --- Order of base time stepping scheme
       ISCHTP =              1 (1: order 1; 2: order 2      )
                                                             

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


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

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 VelocityX             1      1      1      1      0 0.10E+01 0.10E+01
 VelocityY             1      1      1      1      0 0.10E+01 0.10E+01
 VelocityZ             1      1      1      1      0 0.10E+01 0.10E+01
-------------------------------------------------------------

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


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


 ** STOKES
    ------
       IVELCO =              1 (0: segregated solving of the
                                   velocity components during
                                   the prediction step
                                1: coupled solving of the
                                   velocity components       )
       IPHYDR =              0 (1: account for explicit
                                   balance between pressure
                                   gradient, gravity source
                                   terms, and head losses     )
       ICALHY =              0 (1: compute hydrastatic
                                   pressure for Dirichlet
                                   conditions for pressure
                                   on outlet                  )
       IPRCO  =              1 (1: pressure-continuity        )
       IPUCOU =              0 (1: reinforced U-P coupling    )
       NTERUP =              1 (n: n sweeps on navsto for
                                   velocity/pressure coupling )

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.90000E+00 for pressure (relaxation)
       ARAK   =    0.10000E+01 (Arakawa factor              )

       ISTMPF =              1 (time scheme for flow
                               (0: explicit (THETFL = 0     )
                               (1: std scheme (Saturne 1.0  )
                               (2: 2nd-order (THETFL = 0.5  )
       THETFL =   -0.99900E+03 (theta for mass flow         )
       IROEXT =              0 (density extrapolation
                               (0: explicit
                               (1: n+thetro with thetro=1/2
                               (2: n+thetro with thetro=1
       THETRO =    0.00000E+00 (theta for density
                               ((1+theta).new-theta.old
       IVIEXT =              0 (total viscosity extrapolation
                               (0: explicit
                               (1: n+thetvi with thetro=1/2
                               (2: n+thetvi with thetro=1
       THETVI =    0.00000E+00 (theta for total viscosity
                               ((1+theta).new-theta.old
       ICPEXT =              0 (specific heat extrapolation
                               (0: explicit
                               (1: n+thetcp with thetro=1/2
                               (2: n+thetcp with thetro=1
       THETCP =    0.00000E+00 (specific heat theta-scheme
                               ((1+theta).new-theta.old
       THETSN =    0.00000E+00 (Nav-Stokes S.T. theta scheme)
                               ((1+theta).new-theta.old
       THETST =    0.00000E+00 (Turbulence S.T. theta-scheme)
                               ((1+theta).new-theta.old
       EPSUP  =    0.10000E-04 (Velocity/pressure coupling
                                stop test                   )


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


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

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

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityX           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityY           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityZ           100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Pressure              1     -1  0.1500E+01
 VelocityX             1     -1  0.1500E+01
 VelocityY             1     -1  0.1500E+01
 VelocityZ             1     -1  0.1500E+01
-----------------------------------

       NSWRGR =                (nb sweep gradient reconstr. )
       NSWRSM =                (nb sweep rhs reconstrcution )
       EPSRGR =                (grad. reconstruction prec.  )
       EPSRSM =                (rhs   reconstruction prec.  )
       EXTRAG =  [0.;1.]       (gradients extrapolation     )
       IRCFLU =  0 ou  1       (flow reconstruction         )
       IMLIGR =  < 0, 0 ou 1   (gradient limitation method  )
       CLIMGR =  > 1 ou 1      (gradient limitation coeff.  )


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


 ** FACE INTERPOLATION
    ------------------
       IMVISF =              0 (0 arithmetic                )


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


 ** CALCULATION OF TEMPORAL MEANS (MOMENTS)
    ---------------------------------------

       NBMOMT =              0 (Number of moments           )

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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Pressure              0  10000  0.1000E-07      1
 VelocityX            -1  10000  0.1000E-07      1
 VelocityY            -1  10000  0.1000E-07      1
 VelocityZ            -1  10000  0.1000E-07      1
-----------------------------------

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


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


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

       NCEGRM =             30 (Max nb cells coarsest grid  )
       NGRMAX =             25 (Max number of levels        )
--------------------------------------
 Variable           IMGR NCYMAX NITMGF
--------------------------------------                       
 Pressure              1    100     10
 VelocityX             0    100     10
 VelocityY             0    100     10
 VelocityZ             0    100     10
------------------------------

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


  Multigrid coarsening type: algebraic, face traveral by criteria

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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =             40 (Final time step required    )

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


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


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

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

 --- Post-processed variables

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

 --- Probe history files
       NTHIST =             -1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              0 (Number of probes     )
       NTHSAV =             -1 (Checkpoint frequency )

       Number Name                  Nb. probes (-1: all)
         2 Pressure                      -1
         3 VelocityX                     -1
         4 VelocityY                     -1
         5 VelocityZ                     -1
         6 Density                       -1
         7 LamVisc                       -1
         8 CourantNb                     -1
         9 FourierNb                     -1
        10 total_pressure                -1
        11 LocalTime                     -1
         --           --                --

 --- Log files
       NTLIST =              5 (Output frequency     )

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

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

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


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


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

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


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


 Reading file:        mesh_input
 Finished reading:    mesh_input


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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: at calculation end

 Number of cells:                                      47142

 ----------------------------------------------------------
 Number of cells + halo cells:                         47142


 ----------------------------------------------------------
 Number of interior faces:                             89206

 ----------------------------------------------------------
 Number of boundary faces:                             10156

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        619
      2 : [          3 ;          4 ] =      46523

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

 Renumbering mesh:

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


 Matrix bandwidth for volume mesh :          47012
 Matrix profile/lines for volume mesh :      25187

 Mesh coordinates:               minimum    and maximum
                       X : -1.9228667e-02 -9.8470936e-03
                       Y : -3.7284411e-02 -3.0620022e-02
                       Z : -2.9999979e-03  4.0343330e-03
 Mesh
     Number of cells:          47142
     Number of interior faces: 89206
     Number of boundary faces: 10156
     Number of vertices:       10612

 Groups:
    "inlet"
       boundary faces:           52
    "outlet"
       boundary faces:           43
    "walls"
       boundary faces:        10061

 --- Information on the volumes
       Minimum control volume      =  2.1736982e-14
       Maximum control volume      =  1.2389418e-10
       Total volume for the domain =  1.1379424e-07

  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: 1428 -->   3 %

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

  Criterion 5: Guilt by Association:
    Number of bad cells detected: 0 -->   0 %

 Warning:
 --------
    Mesh quality issue has been detected

    The mesh should be re-considered using the listed criteria.

    The calculation will run but the solution quality may be degraded...

 Computing geometric quantities (0.123 s)
                                                             
       ALMAX  =    0.48718E-02 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.


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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Pressure          0.0000E+00  0.0000E+00
  VelocityX         0.0000E+00  0.0000E+00
  VelocityY         0.0000E+00  0.0000E+00
  VelocityZ         0.0000E+00  0.0000E+00
 ---------------------------------

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



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  Density           0.7200E+03  0.7200E+03
  LamVisc           0.4800E-03  0.4800E-03
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          52
Smooth wall               5       10061
Rough wall                6           0
Symmetry                  4           0
Free outlet               3          43
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =   -0.10188E-01  -0.31877E-01   0.19608E-04



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52         0.000000000E+00
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


 TIME FOR THE TIME STEP                1:        0.32823E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271692E-03
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   :  0.52579E-03 0.11720E+00
   Friction velocity        uk    :  0.52579E-03 0.10547E+00
   Dimensionless distance   yplus :  0.19947E-01 0.80554E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       9182
   Total number of wall faces                   :      10061
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH NOT ENOUGH REFINED AT THE WALL            
@    ========                                                
@    The mesh does not seem to be enough refined at the wall 
@      to be able to run a laminar simulation.               
@                                                            
@    The last time step at which too large values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          2
@                                                            
@    The minimum value for yplus must be lower than the      
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight 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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


 TIME FOR THE TIME STEP                2:        0.38994E+01

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


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



   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.20776E-02 0.12413E+00
   Friction velocity        uk    :  0.20776E-02 0.98500E-01
   Dimensionless distance   yplus :  0.38435E-01 0.69756E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       9159
   Total number of wall faces                   :      10061
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH NOT ENOUGH REFINED AT THE WALL            
@    ========                                                
@    The mesh does not seem to be enough refined at the wall 
@      to be able to run a laminar simulation.               
@                                                            
@    The last time step at which too large values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          3
@                                                            
@    The minimum value for yplus must be lower than the      
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight 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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


 TIME FOR THE TIME STEP                3:        0.39412E+01

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


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



 TIME FOR THE TIME STEP                4:        0.40339E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271603E-03
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   :  0.10762E-02 0.12994E+00
   Friction velocity        uk    :  0.10762E-02 0.10585E+00
   Dimensionless distance   yplus :  0.21445E-01 0.90435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       9079
   Total number of wall faces                   :      10061
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10378E-03     786   0.73725E-01   0.35809E+00 
c  VelocityX    0.48495E-04     247   0.36606E+00   0.15400E-01 
c  VelocityY    0.48495E-04     247   0.36606E+00   0.31777E-01 
c  VelocityZ    0.48495E-04     247   0.36606E+00   0.45208E-01 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.18724E+01   0.10261E+03         --         -- 
v  VelocityX   -0.13789E+00   0.46046E+00         --         -- 
v  VelocityY   -0.36422E+00   0.32627E+00         --         -- 
v  VelocityZ   -0.44305E+00   0.34673E+00         --         -- 
v  CourantNb    0.97523E-02   0.26465E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10132E+06   0.10143E+06          0          0 
v  LocalTime    0.10000E-01   0.24366E-01      46989          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.97523E-02 -0.14597E-01 -0.31492E-01  0.20757E-02  
Courant max  0.26465E+03 -0.14931E-01 -0.33220E-01 -0.86794E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.71056E+00 -0.18414E-01 -0.34531E-01  0.28568E-02  
Cou_Fou max  0.29070E+03 -0.14931E-01 -0.33220E-01 -0.86794E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.24366E-01 -0.18359E-01 -0.31002E-01  0.48820E-04  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                5:        0.39713E+01

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


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



 TIME FOR THE TIME STEP                6:        0.38944E+01

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


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



 TIME FOR THE TIME STEP                7:        0.40068E+01

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


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



 TIME FOR THE TIME STEP                8:        0.40543E+01

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


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



 TIME FOR THE TIME STEP                9:        0.40052E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271501E-03
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   :  0.17375E-02 0.13293E+00
   Friction velocity        uk    :  0.17375E-02 0.10900E+00
   Dimensionless distance   yplus :  0.36788E-01 0.11677E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       9024
   Total number of wall faces                   :      10061
------------------------------------------------------------




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


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

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

   ** Writing the auxilliary restart file
      -----------------------------------

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


 Time for restart files:    0.58510E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.87928E-04     592   0.27304E-01   0.15951E+00 
c  VelocityX    0.56089E-04     315   0.35137E+00   0.56205E-02 
c  VelocityY    0.56089E-04     315   0.35137E+00   0.68015E-02 
c  VelocityZ    0.56089E-04     315   0.35137E+00   0.10215E-01 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.18408E+02   0.11463E+03         --         -- 
v  VelocityX   -0.11322E+00   0.51348E+00         --         -- 
v  VelocityY   -0.36648E+00   0.43555E+00         --         -- 
v  VelocityZ   -0.44335E+00   0.42105E+00         --         -- 
v  CourantNb    0.40996E-02   0.26455E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10131E+06   0.10144E+06          0          0 
v  LocalTime    0.10000E-01   0.21436E-01      47002          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.40996E-02 -0.14076E-01 -0.34092E-01  0.28382E-02  
Courant max  0.26455E+03 -0.14931E-01 -0.33220E-01 -0.86794E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.97817E+00 -0.18899E-01 -0.32786E-01  0.21145E-02  
Cou_Fou max  0.29061E+03 -0.14931E-01 -0.33220E-01 -0.86794E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.21436E-01 -0.18304E-01 -0.35998E-01  0.21753E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               10:        0.39566E+01

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


 INSTANT    0.110000000E+01   TIME STEP NUMBER              11
 ============================================================= 



 TIME FOR THE TIME STEP               11:        0.38237E+01

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


 INSTANT    0.120000000E+01   TIME STEP NUMBER              12
 ============================================================= 



 TIME FOR THE TIME STEP               12:        0.40431E+01

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


 INSTANT    0.130000000E+01   TIME STEP NUMBER              13
 ============================================================= 



 TIME FOR THE TIME STEP               13:        0.38831E+01

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


 INSTANT    0.140000000E+01   TIME STEP NUMBER              14
 ============================================================= 



 TIME FOR THE TIME STEP               14:        0.39623E+01

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


 INSTANT    0.150000000E+01   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271459E-03
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   :  0.55910E-03 0.13941E+00
   Friction velocity        uk    :  0.55910E-03 0.98179E-01
   Dimensionless distance   yplus :  0.33516E-01 0.12108E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       8928
   Total number of wall faces                   :      10061
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72834E-04     588   0.15353E-01   0.10039E+00 
c  VelocityX    0.61581E-04     318   0.33367E+00   0.44852E-02 
c  VelocityY    0.61581E-04     318   0.33367E+00   0.42673E-02 
c  VelocityZ    0.61581E-04     318   0.33367E+00   0.76334E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.21290E+02   0.12417E+03         --         -- 
v  VelocityX   -0.14323E+00   0.53136E+00         --         -- 
v  VelocityY   -0.30767E+00   0.46730E+00         --         -- 
v  VelocityZ   -0.45285E+00   0.39295E+00         --         -- 
v  CourantNb    0.29589E-02   0.31748E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10130E+06   0.10145E+06          0          0 
v  LocalTime    0.10000E-01   0.34523E-01      46918          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.29589E-02 -0.14710E-01 -0.30669E-01  0.34292E-03  
Courant max  0.31748E+03 -0.14834E-01 -0.33678E-01 -0.95825E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.69072E+00 -0.17875E-01 -0.36037E-01  0.12048E-02  
Cou_Fou max  0.34647E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.34523E-01 -0.18304E-01 -0.35998E-01  0.21753E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               15:        0.38999E+01

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


 INSTANT    0.160000000E+01   TIME STEP NUMBER              16
 ============================================================= 



 TIME FOR THE TIME STEP               16:        0.40319E+01

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


 INSTANT    0.170000000E+01   TIME STEP NUMBER              17
 ============================================================= 



 TIME FOR THE TIME STEP               17:        0.40571E+01

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


 INSTANT    0.180000000E+01   TIME STEP NUMBER              18
 ============================================================= 



 TIME FOR THE TIME STEP               18:        0.40740E+01

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


 INSTANT    0.190000000E+01   TIME STEP NUMBER              19
 ============================================================= 



 TIME FOR THE TIME STEP               19:        0.41343E+01

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


 INSTANT    0.200000000E+01   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271975E-03
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   :  0.14172E-02 0.15150E+00
   Friction velocity        uk    :  0.14172E-02 0.96927E-01
   Dimensionless distance   yplus :  0.47021E-01 0.11912E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       8869
   Total number of wall faces                   :      10061
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         20, Physical time    0.20000E+01


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

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

   ** Writing the auxilliary restart file
      -----------------------------------

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


 Time for restart files:    0.60700E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69941E-04     566   0.10700E-01   0.80878E-01 
c  VelocityX    0.64458E-04     328   0.32404E+00   0.44163E-02 
c  VelocityY    0.64458E-04     328   0.32404E+00   0.39198E-02 
c  VelocityZ    0.64458E-04     328   0.32404E+00   0.53477E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.23402E+02   0.12974E+03         --         -- 
v  VelocityX   -0.14249E+00   0.58427E+00         --         -- 
v  VelocityY   -0.32911E+00   0.43226E+00         --         -- 
v  VelocityZ   -0.44660E+00   0.42032E+00         --         -- 
v  CourantNb    0.20066E-03   0.36088E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10130E+06   0.10145E+06          0          0 
v  LocalTime    0.10000E-01   0.55599E-01      46844          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.20066E-03 -0.18115E-01 -0.37010E-01  0.83280E-03  
Courant max  0.36088E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.10742E+01 -0.17680E-01 -0.35961E-01  0.17819E-02  
Cou_Fou max  0.39394E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.55599E-01 -0.18542E-01 -0.34726E-01  0.25817E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               20:        0.40316E+01

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


 INSTANT    0.210000000E+01   TIME STEP NUMBER              21
 ============================================================= 



 TIME FOR THE TIME STEP               21:        0.40552E+01

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


 INSTANT    0.220000000E+01   TIME STEP NUMBER              22
 ============================================================= 



 TIME FOR THE TIME STEP               22:        0.40901E+01

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


 INSTANT    0.230000000E+01   TIME STEP NUMBER              23
 ============================================================= 



 TIME FOR THE TIME STEP               23:        0.40208E+01

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


 INSTANT    0.240000000E+01   TIME STEP NUMBER              24
 ============================================================= 



 TIME FOR THE TIME STEP               24:        0.40594E+01

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


 INSTANT    0.250000000E+01   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271978E-03
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   :  0.79272E-03 0.15673E+00
   Friction velocity        uk    :  0.79272E-03 0.97783E-01
   Dimensionless distance   yplus :  0.31521E-01 0.11694E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       8808
   Total number of wall faces                   :      10061
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70497E-04     623   0.75691E-02   0.71872E-01 
c  VelocityX    0.66603E-04     328   0.32693E+00   0.36881E-02 
c  VelocityY    0.66603E-04     328   0.32693E+00   0.29686E-02 
c  VelocityZ    0.66603E-04     328   0.32693E+00   0.44304E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.28314E+02   0.12950E+03         --         -- 
v  VelocityX   -0.17574E+00   0.61607E+00         --         -- 
v  VelocityY   -0.30863E+00   0.47869E+00         --         -- 
v  VelocityZ   -0.45375E+00   0.43823E+00         --         -- 
v  CourantNb    0.30641E-02   0.39243E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10130E+06   0.10145E+06          0          0 
v  LocalTime    0.10000E-01   0.89543E-01      46955          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.30641E-02 -0.13627E-01 -0.35473E-01  0.13007E-02  
Courant max  0.39243E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.10877E+01 -0.18414E-01 -0.34531E-01  0.28568E-02  
Cou_Fou max  0.42549E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.89543E-01 -0.18542E-01 -0.34726E-01  0.25817E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               25:        0.40932E+01

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


 INSTANT    0.260000000E+01   TIME STEP NUMBER              26
 ============================================================= 



 TIME FOR THE TIME STEP               26:        0.39874E+01

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


 INSTANT    0.270000000E+01   TIME STEP NUMBER              27
 ============================================================= 



 TIME FOR THE TIME STEP               27:        0.40008E+01

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


 INSTANT    0.280000000E+01   TIME STEP NUMBER              28
 ============================================================= 



 TIME FOR THE TIME STEP               28:        0.39895E+01

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


 INSTANT    0.290000000E+01   TIME STEP NUMBER              29
 ============================================================= 



 TIME FOR THE TIME STEP               29:        0.38340E+01

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


 INSTANT    0.300000000E+01   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716272101E-03
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   :  0.77748E-03 0.16211E+00
   Friction velocity        uk    :  0.77748E-03 0.10410E+00
   Dimensionless distance   yplus :  0.13692E-01 0.11598E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       8739
   Total number of wall faces                   :      10061
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         30, Physical time    0.30000E+01


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

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

   ** Writing the auxilliary restart file
      -----------------------------------

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


 Time for restart files:    0.61440E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65464E-04     516   0.55478E-02   0.59725E-01 
c  VelocityX    0.68586E-04     325   0.32390E+00   0.28763E-02 
c  VelocityY    0.68586E-04     325   0.32390E+00   0.27541E-02 
c  VelocityZ    0.68586E-04     325   0.32390E+00   0.35577E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.32274E+02   0.12870E+03         --         -- 
v  VelocityX   -0.23599E+00   0.67198E+00         --         -- 
v  VelocityY   -0.30962E+00   0.52877E+00         --         -- 
v  VelocityZ   -0.45511E+00   0.47004E+00         --         -- 
v  CourantNb    0.13344E-01   0.42824E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10129E+06   0.10145E+06          0          0 
v  LocalTime    0.10000E-01   0.55490E-01      46970          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.13344E-01 -0.14711E-01 -0.30662E-01 -0.29540E-03  
Courant max  0.42824E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.13486E+01 -0.18154E-01 -0.34994E-01  0.27608E-02  
Cou_Fou max  0.46130E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.55490E-01 -0.18052E-01 -0.36830E-01  0.12612E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               30:        0.38814E+01

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


 INSTANT    0.310000000E+01   TIME STEP NUMBER              31
 ============================================================= 



 TIME FOR THE TIME STEP               31:        0.39670E+01

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


 INSTANT    0.320000000E+01   TIME STEP NUMBER              32
 ============================================================= 



 TIME FOR THE TIME STEP               32:        0.39316E+01

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


 INSTANT    0.330000000E+01   TIME STEP NUMBER              33
 ============================================================= 



 TIME FOR THE TIME STEP               33:        0.40112E+01

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


 INSTANT    0.340000000E+01   TIME STEP NUMBER              34
 ============================================================= 



 TIME FOR THE TIME STEP               34:        0.39861E+01

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


 INSTANT    0.350000000E+01   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271210E-03
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   :  0.15253E-02 0.16611E+00
   Friction velocity        uk    :  0.15253E-02 0.94736E-01
   Dimensionless distance   yplus :  0.46317E-01 0.11551E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       8696
   Total number of wall faces                   :      10061
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61977E-04     588   0.42679E-02   0.50978E-01 
c  VelocityX    0.70302E-04     323   0.32204E+00   0.24311E-02 
c  VelocityY    0.70302E-04     323   0.32204E+00   0.22842E-02 
c  VelocityZ    0.70302E-04     323   0.32204E+00   0.29128E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.33089E+02   0.13248E+03         --         -- 
v  VelocityX   -0.24603E+00   0.70523E+00         --         -- 
v  VelocityY   -0.34796E+00   0.48572E+00         --         -- 
v  VelocityZ   -0.46225E+00   0.47625E+00         --         -- 
v  CourantNb    0.45414E-02   0.48268E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10129E+06   0.10146E+06          0          0 
v  LocalTime    0.10000E-01   0.56398E-01      46906          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.45414E-02 -0.14508E-01 -0.31973E-01  0.24641E-02  
Courant max  0.48268E+03 -0.14901E-01 -0.33947E-01 -0.96879E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.11655E+01 -0.16851E-01 -0.33790E-01  0.27270E-02  
Cou_Fou max  0.51407E+03 -0.15261E-01 -0.32636E-01 -0.56251E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.56398E-01 -0.18115E-01 -0.37010E-01  0.83280E-03  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               35:        0.39798E+01

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


 INSTANT    0.360000000E+01   TIME STEP NUMBER              36
 ============================================================= 



 TIME FOR THE TIME STEP               36:        0.39874E+01

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


 INSTANT    0.370000000E+01   TIME STEP NUMBER              37
 ============================================================= 



 TIME FOR THE TIME STEP               37:        0.40283E+01

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


 INSTANT    0.380000000E+01   TIME STEP NUMBER              38
 ============================================================= 



 TIME FOR THE TIME STEP               38:        0.39583E+01

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


 INSTANT    0.390000000E+01   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271313E-03
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   :  0.73382E-03 0.17252E+00
   Friction velocity        uk    :  0.73382E-03 0.96913E-01
   Dimensionless distance   yplus :  0.26482E-01 0.11584E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       8667
   Total number of wall faces                   :      10061
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH NOT ENOUGH REFINED AT THE WALL            
@    ========                                                
@    The mesh does not seem to be enough refined at the wall 
@      to be able to run a laminar simulation.               
@                                                            
@    The last time step at which too large values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         39
@                                                            
@    The minimum value for yplus must be lower than the      
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight 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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


 TIME FOR THE TIME STEP               39:        0.38572E+01

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


 INSTANT    0.400000000E+01   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.716271705E-03
Smooth wall               5       10061         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          43         0.716271171E-03
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   :  0.97898E-03 0.17119E+00
   Friction velocity        uk    :  0.97898E-03 0.95796E-01
   Dimensionless distance   yplus :  0.19161E-01 0.11552E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       8679
   Total number of wall faces                   :      10061
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH NOT ENOUGH REFINED AT THE WALL            
@    ========                                                
@    The mesh does not seem to be enough refined at the wall 
@      to be able to run a laminar simulation.               
@                                                            
@    The last time step at which too large values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         40
@                                                            
@    The minimum value for yplus must be lower than the      
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight 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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            



 Write final restart files
   checkpoint at iteration         40, Physical time    0.40000E+01


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

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

   ** Writing the auxilliary restart file
      -----------------------------------

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


 Time for restart files:    0.61390E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59617E-04     556   0.33656E-02   0.44477E-01 
c  VelocityX    0.71700E-04     316   0.32557E+00   0.22868E-02 
c  VelocityY    0.71700E-04     316   0.32557E+00   0.22348E-02 
c  VelocityZ    0.71700E-04     316   0.32557E+00   0.29764E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.34218E+02   0.13745E+03         --         -- 
v  VelocityX   -0.29139E+00   0.77809E+00         --         -- 
v  VelocityY   -0.37536E+00   0.53739E+00         --         -- 
v  VelocityZ   -0.45694E+00   0.48576E+00         --         -- 
v  CourantNb    0.21314E-02   0.56690E+03          0          0 
v  FourierNb    0.24341E+00   0.10141E+03          0          0 
v  total_pressu 0.10129E+06   0.10146E+06          0          0 
v  LocalTime    0.10000E-01   0.67739E-01      46919          0 
---------------------------------------------------------------
  
  

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

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.21314E-02 -0.14617E-01 -0.31172E-01 -0.16720E-02  
Courant max  0.56690E+03 -0.14901E-01 -0.33947E-01 -0.96879E-03  
Fourier min  0.24341E+00 -0.17698E-01 -0.34188E-01 -0.27480E-02  
Fourier max  0.10141E+03 -0.14671E-01 -0.31009E-01  0.13913E-02  
Cou_Fou min  0.12365E+01 -0.18681E-01 -0.33970E-01  0.25929E-02  
Cou_Fou max  0.58817E+03 -0.14901E-01 -0.33947E-01 -0.96879E-03  
---------------------------------------------------------------
Dt min       0.10000E-01 -0.15541E-01 -0.35329E-01  0.14594E-02  
Dt max       0.67739E-01 -0.18209E-01 -0.36507E-01  0.13990E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               40:        0.39234E+01

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.35300E-03
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:            157.894 s
  System CPU time:            0.324 s

  Elapsed time:             158.814 s
  CPU / elapsed time          0.996

Memory use summary:

  Total memory used:                             167.605 MiB
  Theoretical instrumented dynamic memory:        35.571 MiB
