command: 
 ./cs_solver --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.2.2


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

  build Wed 16 Apr 2014 16:41:41 BST
  MPI version 2.1 (Open MPI 1.7.2)


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

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

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


Local case configuration:

  Date:                Wed 23 Apr 2014 14:13:20 BST
  System:              Linux 3.11.6-4-desktop
  Machine:             mbgnhma2lx
  Processor:           model name	: Intel(R) Core(TM) i7-3820 CPU @ 3.60GHz
  Memory:              32187 MB
  User:                mbgnhma2 (mbgnhma2)
  Directory:           /home/mbgnhma2/Code_saturne/Mixer/TurboModule/2D-Mixer-Keps/RESU/20140423-1413
  MPI ranks:           4 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

 Reading metadata from file: "mesh_input/mesh_01"
 Reading metadata from file: "mesh_input/mesh_02"
 Reading metadata from file: "mesh_input/mesh_03"
 Reading metadata from file: "mesh_input/mesh_04"
 Reading metadata from file: "mesh_input/mesh_05"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              6 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )


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


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

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

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

  -- Continuous phase:

       RO0    =    0.99820E+03 (Reference density           )
       VISCL0 =    0.10030E-02 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


 ** THERMAL MODEL
    -------------
 --- Continuous phase:

   - Commons
       ITHERM =              0 (0:  no thermal model        )
                               (10: temperature C           )
                               (11: temperature K           )
                               (20: enthalpy                )
                               (30: total energy            )
       ISCALT =             -1 (Thermal scalar number       )


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

 --- Continuous phase:

   - Commons
       ITURB  =             21 (Turbulence model            )
       IDEUCH =              1 (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)     )

   - Linear production k-epsilon (ITURB = 21)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.17233E+00 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )
       RELAXV =    0.10000E+01 for k        (Relaxation)
       RELAXV =    0.10000E+01 for epsilon  (Relaxation)

   - Rotation/curvature correction
       IRCCOR =              0 (0: desactivated             )
                               (1: activated                )

 --- 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))

   - Linear production k-epsilon (ITURB = 21)
       Ce1    =    0.14400E+01 (Cepsilon 1: production coef.)
       CE2    =    0.19200E+01 (Cepsilon 2: dissipat.  coef.)
       SIGMAK =    0.10000E+01 (Prandtl relative to k       )
       SIGMAE =    0.13000E+01 (Prandtl relative to epsilon )
       CMU    =    0.90000E-01 (Cmu constant                )


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


 ** 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-03 (Minimum time step           )
       DTMAX  =    0.10000E+01 (Maximum time step           )
       DTREF  =    0.10000E-02 (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
 Turb Kinetic Ene      1  0.1000E+01
 Turb Dissipation      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
 Turb Kinetic Ene      1      1      1      1      0 0.00E+00 0.10E+01
 Turb Dissipation      1      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
    ------
       IPHYDR =              0 (1: account for explicit
                                   balance between pressure
                                   gradient, gravity source
                                   terms, and head losses     )
       ICALHY =              0 (1: compute hydrastatic
                                   pressure for Dirichlet
                                   conditions for pressure
                                   on outlet                  )
       IPRCO  =              1 (1: pressure-continuity        )
       IPUCOU =              0 (1: reinforced U-P coupling    )
       NTERUP =              1 (n: n sweeps on navsto for
                                   velocity/pressure coupling )

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

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

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


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


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

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

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityX           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityY           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityZ           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Turb Kinetic Ene    100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Turb Dissipation    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
 Turb Kinetic Ene      1     -1  0.1500E+01
 Turb Dissipation      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             -1  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
 Turb Kinetic Ene     -1  10000  0.1000E-07      1
 Turb Dissipation     -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              0    100     10
 VelocityX             0    100     10
 VelocityY             0    100     10
 VelocityZ             0    100     10
 Turb Kinetic Ene      0    100     10
 Turb Dissipation      0    100     10
------------------------------

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


  Multigrid rank merge parameters:
    mean  coarse cells merge threshold: 300
    total coarse cells merge threshold: 500
    minimum ranks merge threshold:      1
    merge stride:                       1

  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 =             50 (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       
         6 Turb Kinetic Ene
         7 Turb Dissipation
         8 Density         
        10 Turb Viscosity  
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              4 (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 Turb Kinetic Ene              -1
         7 Turb Dissipation              -1
        10 Turb Viscosity                -1
         --           --                --

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

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

         2 Pressure                       2
         3 VelocityX                      2
         4 VelocityY                      2
         5 VelocityZ                      2
         6 Turb Kinetic Ene               1
         7 Turb Dissipation               1
        10 Turb Viscosity              -999
        11 CFL                         -999
        12 Fourier Number              -999
         --           --                --

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


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


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

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


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


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: 
      time dependency: transient connectivity
      output: every 25 time steps and at calculation end


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

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

 Reading file:        mesh_input/mesh_03
 Finished reading:    mesh_input/mesh_03

 Reading file:        mesh_input/mesh_04
 Finished reading:    mesh_input/mesh_04

 Reading file:        mesh_input/mesh_05
 Finished reading:    mesh_input/mesh_05
 No "partition_input/domain_number_4" file available;

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [      44711 ;      44712 ] =          4

 Writing file:        partition_output/domain_number_4
 Finished writing:    partition_output/domain_number_4

 Partitioning finished (1.23 s)


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

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

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

 Histogram of the number of cells per rank:

    minimum value =              44711
    maximum value =              44712

      1 : [      44711 ;      44712 ] =          4

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

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

    minimum value =              45075
    maximum value =              45141

      1 : [      45075 ;      45088 [ =          1
      2 : [      45088 ;      45101 [ =          1
      3 : [      45101 ;      45114 [ =          0
      4 : [      45114 ;      45127 [ =          1
      5 : [      45127 ;      45141 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =                364
    maximum value =                430

      1 : [        364 ;        377 [ =          1
      2 : [        377 ;        390 [ =          1
      3 : [        390 ;        403 [ =          0
      4 : [        403 ;        416 [ =          1
      5 : [        416 ;        430 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =              87138
    maximum value =              87177

      1 : [      87138 ;      87145 [ =          2
      2 : [      87145 ;      87153 [ =          0
      3 : [      87153 ;      87161 [ =          0
      4 : [      87161 ;      87169 [ =          0
      5 : [      87169 ;      87177 ] =          2

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

 Histogram of the number of boundary faces per rank:

    minimum value =              93366
    maximum value =              93451

      1 : [      93366 ;      93383 [ =          1
      2 : [      93383 ;      93400 [ =          0
      3 : [      93400 ;      93417 [ =          1
      4 : [      93417 ;      93434 [ =          1
      5 : [      93434 ;      93451 ] =          1

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =       2016
      2 : [          3 ;          4 ] =     176829

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  2
    maximum value =                  3

      1 : [          2 ;          3 ] =          4

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

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

 Writing file:        mesh_output
 Finished writing:    mesh_output

 Renumbering mesh:

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


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =              44821
    maximum value =              44915

      1 : [      44821 ;      44839 [ =          1
      2 : [      44839 ;      44858 [ =          0
      3 : [      44858 ;      44877 [ =          0
      4 : [      44877 ;      44896 [ =          0
      5 : [      44896 ;      44915 ] =          3

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               1338
    maximum value =               1916

      1 : [       1338 ;       1453 [ =          1
      2 : [       1453 ;       1569 [ =          1
      3 : [       1569 ;       1684 [ =          0
      4 : [       1684 ;       1800 [ =          0
      5 : [       1800 ;       1916 ] =          2

 Mesh coordinates:               minimum    and maximum
                       X : -4.9222948e-02  4.9222948e-02
                       Y : -4.9215902e-02  4.9217488e-02
                       Z :  0.0000000e+00  1.0000000e-02
 Mesh
     Number of cells:          178845
     Number of interior faces: 347724
     Number of boundary faces: 373638
     Number of vertices:       369362

 Groups:
    "fluid_gap1"
       cells:                 14400
    "fluid_gap2"
       cells:                 31824
    "fluid_holes"
       cells:                  6432
    "fluid_inlet"
       cells:                  3800
    "fluid_outside1"
       cells:                 14174
    "fluid_outside2"
       cells:                 26498
    "fluid_rotor1"
       cells:                 34489
    "fluid_rotor2"
       cells:                 47228
    "inlet"
       boundary faces:          380
    "interface1"
       boundary faces:          760
    "interface2"
       boundary faces:         2400
    "interface3"
       boundary faces:         1552
    "interface4"
       boundary faces:         4032
    "outlet"
       boundary faces:           11
    "outlet_wall"
       boundary faces:          145
    "rotor1_wall"
       boundary faces:         1212
    "rotor2_wall"
       boundary faces:          968
    "stator_wall"
       interior faces:          800
       boundary faces:         4488
    "symmetry1"
       boundary faces:       178845
    "symmetry2"
       boundary faces:       178845

 --- Information on the volumes
       Minimum control volume      =  1.1740955e-11
       Maximum control volume      =  3.1779964e-08
       Total volume for the domain =  6.5027603e-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: 31 -->   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 %

 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 (0.0881 s)
                                                             
       ALMAX  =    0.40342E-01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  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
  Turb Kinetic Ene  0.1782E-04  0.1782E-04
  Turb Dissipation  0.1678E-06  0.1678E-06
 ---------------------------------

  Local Time Step   0.1000E-02  0.1000E-02
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-02   TIME STEP NUMBER               1
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            

 REINITIALISATION DE LA PRESSION A L'ITERATION          1

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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1700E+00  0.1700E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.0000E+00 IN -0.3205E-01 -0.3474E-03  0.5000E-02
 COURANT MIN=  0.0000E+00 IN -0.3205E-01 -0.3474E-03  0.5000E-02

 FOURIER MAX=  0.1626E+04 IN  0.2246E-01 -0.2252E-01  0.5000E-02
 FOURIER MIN=  0.1767E+00 IN  0.4840E-01  0.2515E-02  0.5000E-02

 COU/FOU MAX=  0.1626E+04 IN  0.2246E-01 -0.2252E-01  0.5000E-02
 COU/FOU MIN=  0.1767E+00 IN  0.4840E-01  0.2515E-02  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =   -0.18302E-02   0.49183E-01   0.50000E-02



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380         0.000000000E+00
Smooth wall               5        6813         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         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 0.87245E+00
   Friction velocity        uet   :  0.00000E+00 0.13875E+00
   Friction velocity        uk    :  0.14256E-03 0.23498E+00
   Dimensionless distance   yplus :  0.14150E-02 0.11250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       5373
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          1
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 6, residue norm: 8.853339e-07, norm: 4.772334e+05, var: Var.  2
 velocity :    1038496 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :  4833, res_abs :  2.3341e-09, res_nor :  9.9982e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 6, residue norm: 9.825239e-07, norm: 3.586322e+05, var: Var.  2
 velocity :      80646 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.2438E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.594858E-01
 _iterative_vector_gradient: isweep = 6, residue norm: 9.825239e-07, norm: 3.579866e+08, var: Var.  2
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.594775E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3456, res_abs :  5.9050e-10, res_nor :  9.9267e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1582e-06; norm:  1.6880e-01
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.777629E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3194, res_abs :  5.8916e-10, res_nor :  9.9042e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2089e-06; norm:  1.6916e-01
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.119256E-01, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1582e-06; norm:  1.6880e-01
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2089e-06; norm:  1.6916e-01

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.2375E+05 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.165E-01 -0.969E-02  0.500E-02

 Max. velocity at interior face  0.1100E+02 ; min. -0.1198E+02
 Max. velocity at boundary face  0.6971E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415649E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59477E-01    6650   0.20048E+00   0.99986E+00 
c  VelocityX    0.23345E+00    4833   0.11391E+00   0.29275E+03 
c  VelocityY    0.23345E+00    4833   0.11391E+00   0.30023E+03 
c  VelocityZ    0.23345E+00    4833   0.11391E+00   0.36514E-12 
c  Turb Kinetic 0.94870E-02    1251   0.48686E-01   0.16380E-01 
c  Turb Dissipa 0.10360E+03    4042   0.22572E+00   0.38149E+08 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation   


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                      -6037           23746          9204.8          8116.4
v  Velocity[x]                 -7.6942           7.567     -0.00092971     -0.00064826
v  Velocity[y]                 -9.0878          10.371        0.050791          0.0532
v  Velocity[z]             -9.9147e-06      1.3017e-05      2.5911e-10     -1.9987e-10
v  Turb Kinetic Energy      1.0406e-07         0.14032       0.0016885      0.00064776
v  Turb Dissipation         1.6781e-07           36888          60.891          19.245
v  Turb Viscosity              0.16999         0.16999         0.16999         0.16999
v  CFL                               0               0               0               0
v  Fourier Number              0.17674          1625.9          222.96          25.075


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.17674          1625.9          222.96          25.075


 TIME FOR THE TIME STEP                1:        0.22793E+02

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


 INSTANT    0.200000000E-02   TIME STEP NUMBER               2
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            

 REINITIALISATION DE LA PRESSION A L'ITERATION          2

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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.2623E-14  0.1700E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.4537E+03 IN  0.1647E-01  0.9693E-02  0.5000E-02
 COURANT MIN=  0.7872E-03 IN  0.4826E-01 -0.5448E-02  0.5000E-02

 FOURIER MAX=  0.2632E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.2524E-01 IN -0.1476E-02  0.3388E-01  0.5000E-02

 COU/FOU MAX=  0.4579E+03 IN  0.1647E-01  0.9693E-02  0.5000E-02
 COU/FOU MIN=  0.1353E+00 IN -0.1460E-01  0.3599E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.194648171E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884351E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.706060e-06, norm: 4.446838e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10412E+02 0.44367E+00
   Friction velocity        uet   :  0.11731E-03 0.99575E+00
   Friction velocity        uk    :  0.10070E-02 0.99363E+00
   Dimensionless distance   yplus :  0.96580E-01 0.20119E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3915
   Nb of faces within the viscous sub-layer     :        734
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          2
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.318472e-06, norm: 4.244180e+06, var: Var.  2
 velocity :     366515 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   365, res_abs :  1.8603e-09, res_nor :  9.9530e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 5.019397e-06, norm: 1.666935e+06, var: Var.  2
 velocity :     299738 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.6898E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.110291E+00
 _iterative_vector_gradient: isweep = 5, residue norm: 5.019397e-06, norm: 1.663935e+09, var: Var.  2
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.110013E+00, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3334, res_abs :  1.1016e-09, res_nor :  9.9883e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.3533e-07; norm:  6.4599e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.364910E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3011, res_abs :  1.0956e-09, res_nor :  9.9337e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.9461e-07; norm:  6.4535e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.564190E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.3533e-07; norm:  6.4599e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.9461e-07; norm:  6.4535e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5759E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.165E-01 -0.969E-02  0.500E-02

 Max. velocity at interior face  0.7409E+01 ; min. -0.7948E+01
 Max. velocity at boundary face  0.5460E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415644E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.11001E+00    6345   0.51155E-01   0.99747E+00 
c  VelocityX    0.18691E+00     365   0.68516E+00   0.20923E+02 
c  VelocityY    0.18691E+00     365   0.68516E+00   0.20995E+02 
c  VelocityZ    0.18691E+00     365   0.68516E+00   0.14188E-12 
c  Turb Kinetic 0.28913E-02     118   0.10010E-02   0.15834E-01 
c  Turb Dissipa 0.47017E+03      53   0.39099E-03   0.48312E+08 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -0.00012311                            20
a  Turb Dissipation           -0.91315                            41


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5758.5          4496.8          868.78          731.44
v  Velocity[x]                 -5.5595          5.8733      0.00021406     -0.00058139
v  Velocity[y]                 -6.2962          7.3279        0.046125        0.053833
v  Velocity[z]             -3.4042e-06      5.8641e-06     -4.1308e-11     -2.0499e-10
v  Turb Kinetic Energy      4.1462e-13         0.19609      0.00059896      0.00015145
v  Turb Dissipation         1.1087e-07           27890          31.261          3.4838
v  Turb Viscosity           2.6232e-15         0.16999         0.01001        0.073935
v  CFL                      0.00078725          453.72          15.609          4.4601
v  Fourier Number             0.025237          26.317          1.6856          1.2867


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.13532          457.89          17.295          5.7469


 TIME FOR THE TIME STEP                2:        0.60805E+01

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


 INSTANT    0.300000000E-02   TIME STEP NUMBER               3
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.7310E-19  0.1717E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.3298E+03 IN  0.1647E-01  0.9693E-02  0.5000E-02
 COURANT MIN=  0.1272E-02 IN  0.4700E-01 -0.5284E-02  0.5000E-02

 FOURIER MAX=  0.2470E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1255E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.3339E+03 IN  0.1647E-01  0.9693E-02  0.5000E-02
 COU/FOU MIN=  0.1048E-01 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.9461e-07; norm:  6.4535e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.121419814E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884356E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 4.804406e-06, norm: 2.789327e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64520E+01 0.45147E+00
   Friction velocity        uet   :  0.74244E-04 0.69867E+00
   Friction velocity        uk    :  0.89491E-03 0.74296E+00
   Dimensionless distance   yplus :  0.89009E-02 0.17489E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2601
   Nb of faces within the viscous sub-layer     :       1630
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          3
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.9615e-07; norm:  6.4431e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 5.029290e-06, norm: 2.664262e+06, var: Var.  2
 velocity :     324627 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   296, res_abs :  1.7041e-09, res_nor :  9.5912e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.955167e-06, norm: 1.896807e+06, var: Var.  2
 velocity :     268897 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4412E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.173952E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.9615e-07; norm:  6.4431e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.989599e-06, norm: 2.942684e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.9615e-07; norm:  6.4431e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.856934E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3235, res_abs :  1.7196e-09, res_nor :  9.8853e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.3491e-06; norm:  3.5625e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.225685E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2927, res_abs :  1.7391e-09, res_nor :  9.9974e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.6225e-06; norm:  3.5067e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.346498E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.3491e-06; norm:  3.5625e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.6225e-06; norm:  3.5067e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.7716E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.290E-01 -0.119E-01  0.500E-02

 Max. velocity at interior face  0.6727E+01 ; min. -0.6486E+01
 Max. velocity at boundary face  0.4763E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415656E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.85693E-01    6162   0.19919E-01   0.49263E+00 
c  VelocityX    0.17768E+00     296   0.34421E+00   0.15640E+02 
c  VelocityY    0.17768E+00     296   0.34421E+00   0.15765E+02 
c  VelocityZ    0.17768E+00     296   0.34421E+00   0.31363E-13 
c  Turb Kinetic 0.17832E-02     110   0.16114E-03   0.12234E-02 
c  Turb Dissipa 0.23870E+03      44   0.45352E-04   0.90207E+07 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -4.4921e-06                            31
a  Turb Dissipation          -0.070956                            32


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -7715.9          4422.8          622.84          587.86
v  Velocity[x]                 -4.7231          4.6946       0.0014463     -0.00048875
v  Velocity[y]                 -4.5537          4.7026        0.041084        0.053887
v  Velocity[z]             -3.9015e-07       2.105e-06     -9.7652e-11     -1.9971e-10
v  Turb Kinetic Energy      1.5315e-18        0.067613      0.00024536       6.805e-05
v  Turb Dissipation         2.3234e-10          7849.7          9.6163         0.71994
v  Turb Viscosity           7.3096e-20         0.17165       0.0062542        0.039811
v  CFL                       0.0012721          329.83          14.393          4.1664
v  Fourier Number            0.0012548          24.698          1.5296         0.86316


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010476          333.87          15.923          5.0296


 TIME FOR THE TIME STEP                3:        0.58380E+01

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


 INSTANT    0.400000000E-02   TIME STEP NUMBER               4
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.2204E-25  0.1732E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2345E+03 IN  0.1647E-01  0.9693E-02  0.5000E-02
 COURANT MIN=  0.3275E-02 IN -0.2445E-01 -0.4206E-01  0.5000E-02

 FOURIER MAX=  0.2362E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1255E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2384E+03 IN  0.1647E-01  0.9693E-02  0.5000E-02
 COU/FOU MIN=  0.8874E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.5704e-06; norm:  8.1911e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.213261382E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884344E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.770733e-06, norm: 1.986558e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54731E+01 0.42599E+00
   Friction velocity        uet   :  0.11171E-02 0.43116E+00
   Friction velocity        uk    :  0.14214E-02 0.55285E+00
   Dimensionless distance   yplus :  0.54886E-01 0.14739E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2521
   Nb of faces within the viscous sub-layer     :       2089
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          4
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.5717e-06; norm:  8.1897e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.841169e-06, norm: 1.950069e+06, var: Var.  2
 velocity :     290023 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   276, res_abs :  1.7773e-09, res_nor :  9.8857e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.859260e-06, norm: 1.995993e+06, var: Var.  2
 velocity :     250620 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5042E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.199725E+00
 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.5717e-06; norm:  8.1897e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.610720e-06, norm: 3.608918e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.5717e-06; norm:  8.1897e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.788017E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3211, res_abs :  1.9791e-09, res_nor :  9.9092e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.1434e-06; norm:  3.1189e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.178025E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2868, res_abs :  1.9863e-09, res_nor :  9.9453e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.3939e-06; norm:  3.0932e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.245997E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.1434e-06; norm:  3.1189e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.3939e-06; norm:  3.0932e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.7487E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.290E-01 -0.119E-01  0.500E-02

 Max. velocity at interior face  0.5713E+01 ; min. -0.5625E+01
 Max. velocity at boundary face  0.4644E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415652E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.78802E-01    6079   0.12317E-01   0.39455E+00 
c  VelocityX    0.17978E+00     276   0.28039E+00   0.10472E+02 
c  VelocityY    0.17978E+00     276   0.28039E+00   0.10563E+02 
c  VelocityZ    0.17978E+00     276   0.28039E+00   0.11142E-13 
c  Turb Kinetic 0.11332E-02     105   0.11347E-03   0.11036E-03 
c  Turb Dissipa 0.12106E+03      61   0.54695E-04   0.42747E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -9.7562e-06                            17
a  Turb Dissipation          -0.088034                            33


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -7487.5          3640.4          333.12          385.53
v  Velocity[x]                 -4.4428          4.3955       0.0029644      -0.0003748
v  Velocity[y]                 -4.2054          4.4024        0.037698        0.053863
v  Velocity[z]              -1.496e-06      1.8399e-06     -9.5809e-11     -1.8522e-10
v  Turb Kinetic Energy      1.2192e-23        0.057324       0.0001846      6.0871e-05
v  Turb Dissipation         5.1788e-16          5280.3          5.6685         0.45428
v  Turb Viscosity           2.2041e-26         0.17324       0.0056905        0.035956
v  CFL                       0.0032752          234.49          13.362          3.9775
v  Fourier Number            0.0012553          23.622          1.5067         0.79898


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0088737          238.43          14.869          4.7765


 TIME FOR THE TIME STEP                4:        0.56485E+01

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


 INSTANT    0.500000000E-02   TIME STEP NUMBER               5
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.9128E-29  0.4576E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2260E+03 IN  0.1569E-01  0.2767E-01  0.5000E-02
 COURANT MIN=  0.2332E-02 IN -0.1914E-01 -0.4471E-01  0.5000E-02

 FOURIER MAX=  0.2301E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1256E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2353E+03 IN  0.1569E-01  0.2767E-01  0.5000E-02
 COU/FOU MIN=  0.6823E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.6414e-06; norm:  8.1481e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.669404836E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884348E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.158761e-06, norm: 1.870879e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56810E+01 0.41997E+00
   Friction velocity        uet   :  0.49241E-04 0.42574E+00
   Friction velocity        uk    :  0.10038E-02 0.51548E+00
   Dimensionless distance   yplus :  0.53555E-01 0.14146E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2382
   Nb of faces within the viscous sub-layer     :       2567
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          5
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.6424e-06; norm:  8.1471e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.182119e-06, norm: 1.855816e+06, var: Var.  2
 velocity :     276619 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   246, res_abs :  1.7340e-09, res_nor :  9.6367e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.104419e-06, norm: 1.903152e+06, var: Var.  2
 velocity :     247818 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5141E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.217032E+00
 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.6424e-06; norm:  8.1471e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.934207e-06, norm: 3.884752e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.6424e-06; norm:  8.1471e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.720044E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3086, res_abs :  2.1500e-09, res_nor :  9.9065e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.0725e-06; norm:  2.6473e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.139520E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2872, res_abs :  2.1683e-09, res_nor :  9.9909e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.5617e-06; norm:  2.5844e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.247826E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.0725e-06; norm:  2.6473e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.5617e-06; norm:  2.5844e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.7153E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.150E-01 -0.274E-01  0.500E-02

 Max. velocity at interior face  0.5447E+01 ; min. -0.5616E+01
 Max. velocity at boundary face  0.4450E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415653E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72004E-01    5958   0.11419E-01   0.33177E+00 
c  VelocityX    0.17994E+00     246   0.26395E+00   0.68756E+01 
c  VelocityY    0.17994E+00     246   0.26395E+00   0.70137E+01 
c  VelocityZ    0.17994E+00     246   0.26395E+00   0.86266E-14 
c  Turb Kinetic 0.94705E-03     113   0.10503E-03   0.54973E-04 
c  Turb Dissipa 0.90974E+02      62   0.51129E-04   0.13921E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -5.1558e-06                             8
a  Turb Dissipation          -0.029059                            28


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -7153.3          3518.5          222.57          283.73
v  Velocity[x]                 -4.5042          4.6664       0.0043973     -0.00026419
v  Velocity[y]                 -4.6065          4.4537        0.035336        0.053831
v  Velocity[z]             -3.0277e-07      1.9441e-06     -4.0375e-11     -1.5528e-10
v  Turb Kinetic Energy      2.8217e-22        0.054749      0.00017203      6.2672e-05
v  Turb Dissipation         1.8944e-19            4669          4.5355         0.39081
v  Turb Viscosity           9.1275e-30          0.4576       0.0052854        0.033411
v  CFL                       0.0023318          226.05          12.752          3.8584
v  Fourier Number            0.0012559          23.011          1.4893         0.75255


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0068228          235.27          14.241          4.6109


 TIME FOR THE TIME STEP                5:        0.54850E+01

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


 INSTANT    0.600000000E-02   TIME STEP NUMBER               6
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3776E-22  0.3574E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2240E+03 IN  0.1569E-01  0.2767E-01  0.5000E-02
 COURANT MIN=  0.1286E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

 FOURIER MAX=  0.2259E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1257E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2331E+03 IN  0.1569E-01  0.2767E-01  0.5000E-02
 COU/FOU MIN=  0.5001E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.8234e-06; norm:  8.1012e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.107628235E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884347E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.977509e-06, norm: 1.873126e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57964E+01 0.41784E+00
   Friction velocity        uet   :  0.79706E-03 0.42421E+00
   Friction velocity        uk    :  0.15245E-02 0.48597E+00
   Dimensionless distance   yplus :  0.55936E-01 0.13103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2315
   Nb of faces within the viscous sub-layer     :       2745
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          6
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.8242e-06; norm:  8.1004e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.996815e-06, norm: 1.862127e+06, var: Var.  2
 velocity :     266750 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   229, res_abs :  1.8136e-09, res_nor :  9.9876e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.253538e-06, norm: 1.941879e+06, var: Var.  2
 velocity :     246402 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4979E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.232161E+00
 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.8242e-06; norm:  8.1004e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 4.217404e-06, norm: 3.963267e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.8242e-06; norm:  8.1004e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.605965E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3099, res_abs :  2.2889e-09, res_nor :  9.8593e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  7.8112e-06; norm:  2.0928e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.117135E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2776, res_abs :  2.3208e-09, res_nor :  9.9966e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.2535e-06; norm:  2.0558e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.205301E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  7.8112e-06; norm:  2.0928e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.2535e-06; norm:  2.0558e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.6795E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.151E-01 -0.275E-01  0.500E-02

 Max. velocity at interior face  0.5796E+01 ; min. -0.5766E+01
 Max. velocity at boundary face  0.4227E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415644E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60596E-01    5875   0.88431E-02   0.26101E+00 
c  VelocityX    0.18159E+00     229   0.23783E+00   0.53054E+01 
c  VelocityY    0.18159E+00     229   0.23783E+00   0.54612E+01 
c  VelocityZ    0.18159E+00     229   0.23783E+00   0.63469E-14 
c  Turb Kinetic 0.86219E-03     127   0.11607E-03   0.55236E-04 
c  Turb Dissipa 0.78173E+02      69   0.47002E-04   0.15276E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -5.7448e-06                             5
a  Turb Dissipation          -0.056004                            27


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -6794.5          3636.8          146.17          212.29
v  Velocity[x]                 -4.9135          5.0777       0.0052529     -0.00019751
v  Velocity[y]                 -4.9889          4.8592        0.033204        0.053853
v  Velocity[z]             -3.0104e-07      9.2552e-07      2.4144e-11      -1.176e-10
v  Turb Kinetic Energy      8.2772e-13         0.05563      0.00017167      6.7203e-05
v  Turb Dissipation          9.083e-12          4226.4          4.0123         0.36447
v  Turb Viscosity           3.7759e-23         0.35744       0.0049503        0.030886
v  CFL                       0.0012863          223.98          12.262          3.7536
v  Fourier Number            0.0012567          22.595          1.4785         0.71432


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0050014          233.14           13.74          4.4679


 TIME FOR THE TIME STEP                6:        0.55192E+01

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


 INSTANT    0.700000000E-02   TIME STEP NUMBER               7
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1624E-15  0.1751E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2213E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COURANT MIN=  0.4289E-03 IN -0.2090E-01 -0.4383E-01  0.5000E-02

 FOURIER MAX=  0.2230E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1258E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2304E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COU/FOU MIN=  0.4084E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.9212e-06; norm:  8.1414e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.659482918E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884356E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.450779e-06, norm: 1.909838e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57446E+01 0.41829E+00
   Friction velocity        uet   :  0.33289E-03 0.41995E+00
   Friction velocity        uk    :  0.11124E-02 0.51378E+00
   Dimensionless distance   yplus :  0.17061E-01 0.13097E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2222
   Nb of faces within the viscous sub-layer     :       2700
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          7
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.9217e-06; norm:  8.1410e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.433024e-06, norm: 1.898378e+06, var: Var.  2
 velocity :     264307 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   222, res_abs :  1.7472e-09, res_nor :  9.4731e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.752916e-06, norm: 1.973210e+06, var: Var.  2
 velocity :     247608 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5355E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.240745E+00
 _iterative_scalar_gradient; variable: pressure; converged in 4 sweeps
                             normed residual:  9.9217e-06; norm:  8.1410e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 4.001792e-06, norm: 3.941006e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.9217e-06; norm:  8.1410e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.529002E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3158, res_abs :  2.3857e-09, res_nor :  9.9096e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.6033e-06; norm:  1.7718e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.115560E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2785, res_abs :  2.3869e-09, res_nor :  9.9145e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  8.9608e-06; norm:  1.7560e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.155966E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.6033e-06; norm:  1.7718e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  8.9608e-06; norm:  1.7560e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.6235E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.301E-01 -0.874E-02  0.500E-02

 Max. velocity at interior face  0.5355E+01 ; min. -0.5772E+01
 Max. velocity at boundary face  0.4215E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415658E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.52900E-01    5943   0.64785E-02   0.21974E+00 
c  VelocityX    0.18444E+00     222   0.20701E+00   0.51566E+01 
c  VelocityY    0.18444E+00     222   0.20701E+00   0.52653E+01 
c  VelocityZ    0.18444E+00     222   0.20701E+00   0.50656E-14 
c  Turb Kinetic 0.83560E-03     135   0.16849E-03   0.47099E-04 
c  Turb Dissipa 0.69677E+02      72   0.46576E-04   0.12342E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -4.3752e-06                             5
a  Turb Dissipation          -0.045957                            29


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -6234.8          3409.4           58.04          144.35
v  Velocity[x]                 -4.5229          4.5747       0.0054863     -0.00019868
v  Velocity[y]                 -4.4803          4.5179        0.031497        0.053868
v  Velocity[z]             -3.3133e-07      1.0581e-06      9.3754e-11      -7.566e-11
v  Turb Kinetic Energy      2.0112e-10          0.0611      0.00018393      7.4888e-05
v  Turb Dissipation         7.5956e-08          3951.3          3.7682         0.35877
v  Turb Viscosity           1.6239e-16         0.17514       0.0046664        0.028715
v  CFL                       0.0004289           221.3          11.896          3.6927
v  Fourier Number            0.0012577          22.299          1.4703         0.68181


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0040838           230.4          13.366          4.3745


 TIME FOR THE TIME STEP                7:        0.54813E+01

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


 INSTANT    0.800000000E-02   TIME STEP NUMBER               8
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3036E-10  0.1758E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2226E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COURANT MIN=  0.7427E-03 IN -0.1914E-01 -0.4471E-01  0.5000E-02

 FOURIER MAX=  0.2209E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1259E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2317E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COU/FOU MIN=  0.4810E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  7.5443e-07; norm:  8.1308e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.215567375E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884342E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.681297e-06, norm: 1.915165e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45832E+01 0.42263E+00
   Friction velocity        uet   :  0.41100E-04 0.37578E+00
   Friction velocity        uk    :  0.91955E-03 0.43987E+00
   Dimensionless distance   yplus :  0.22632E-01 0.12289E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2135
   Nb of faces within the viscous sub-layer     :       2446
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          8
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  7.5446e-07; norm:  8.1305e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.710789e-06, norm: 1.899001e+06, var: Var.  2
 velocity :     263686 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   225, res_abs :  1.8291e-09, res_nor :  9.7781e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.930651e-06, norm: 2.024840e+06, var: Var.  2
 velocity :     250373 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5552E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.240980E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  7.5446e-07; norm:  8.1305e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.882362e-06, norm: 3.828341e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  7.5446e-07; norm:  8.1305e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.503001E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3168, res_abs :  2.3877e-09, res_nor :  9.9081e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 4 sweeps
                             normed residual:  9.7693e-06; norm:  1.6212e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.105734E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2772, res_abs :  2.3926e-09, res_nor :  9.9288e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  7.5349e-07; norm:  1.6122e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.140808E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 4 sweeps
                             normed residual:  9.7693e-06; norm:  1.6212e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  7.5349e-07; norm:  1.6122e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5528E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.282E-01 -0.121E-01  0.500E-02

 Max. velocity at interior face  0.5257E+01 ; min. -0.5305E+01
 Max. velocity at boundary face  0.4295E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415637E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.50300E-01    5940   0.58431E-02   0.20873E+00 
c  VelocityX    0.18706E+00     225   0.19388E+00   0.53740E+01 
c  VelocityY    0.18706E+00     225   0.19388E+00   0.54183E+01 
c  VelocityZ    0.18706E+00     225   0.19388E+00   0.83567E-14 
c  Turb Kinetic 0.83081E-03     141   0.21915E-03   0.80907E-04 
c  Turb Dissipa 0.60337E+02      79   0.53130E-04   0.31043E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -6.7908e-06                             4
a  Turb Dissipation          -0.044334                            23


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5528.3          3013.4         -16.953          90.443
v  Velocity[x]                 -3.9581          4.1316       0.0052984     -0.00021861
v  Velocity[y]                 -4.0161          3.8382        0.030549        0.053897
v  Velocity[z]             -5.6287e-07      1.5235e-06      1.6087e-10     -3.3957e-11
v  Turb Kinetic Energy      4.0253e-10        0.084112      0.00022116      8.6576e-05
v  Turb Dissipation         1.7861e-07          7053.6          4.7512         0.42997
v  Turb Viscosity           3.0356e-11         0.17578       0.0044232        0.026901
v  CFL                      0.00074271          222.55           11.65          3.6692
v  Fourier Number            0.0012589          22.095          1.4665         0.65407


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0048102          231.66          13.116          4.3233


 TIME FOR THE TIME STEP                8:        0.57565E+01

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


 INSTANT    0.900000000E-02   TIME STEP NUMBER               9
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.2032E-11  0.1762E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2213E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COURANT MIN=  0.3513E-03 IN -0.1914E-01 -0.4471E-01  0.5000E-02

 FOURIER MAX=  0.2197E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1260E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2304E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COU/FOU MIN=  0.5587E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  7.7315e-07; norm:  8.0692e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.124120597E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884363E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.857351e-06, norm: 1.953301e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36318E+01 0.42860E+00
   Friction velocity        uet   :  0.64304E-03 0.33350E+00
   Friction velocity        uk    :  0.12741E-02 0.42421E+00
   Dimensionless distance   yplus :  0.29282E-01 0.12173E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2036
   Nb of faces within the viscous sub-layer     :       2339
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          9
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  7.7316e-07; norm:  8.0691e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.886546e-06, norm: 1.938774e+06, var: Var.  2
 velocity :     265561 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   230, res_abs :  1.8681e-09, res_nor :  9.8179e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.258621e-06, norm: 2.049285e+06, var: Var.  2
 velocity :     254001 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.6086E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.236161E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  7.7316e-07; norm:  8.0691e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.791220e-06, norm: 3.708179e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  7.7316e-07; norm:  8.0691e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.493895E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3081, res_abs :  2.3420e-09, res_nor :  9.9169e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  8.5986e-07; norm:  1.5685e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.946670E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2792, res_abs :  2.3344e-09, res_nor :  9.8850e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  8.9130e-07; norm:  1.5587e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.142888E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.5986e-07; norm:  1.5685e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.9130e-07; norm:  1.5587e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5037E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.119E-01 -0.287E-01  0.500E-02

 Max. velocity at interior face  0.4633E+01 ; min. -0.4587E+01
 Max. velocity at boundary face  0.4313E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415660E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.49389E-01    5873   0.60505E-02   0.20913E+00 
c  VelocityX    0.19027E+00     230   0.19292E+00   0.54092E+01 
c  VelocityY    0.19027E+00     230   0.19292E+00   0.55086E+01 
c  VelocityZ    0.19027E+00     230   0.19292E+00   0.11107E-13 
c  Turb Kinetic 0.90241E-03     143   0.22221E-03   0.11479E-03 
c  Turb Dissipa 0.62443E+02      99   0.50006E-04   0.49444E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy      -6.368e-06                             4
a  Turb Dissipation          -0.040352                            28


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5036.6          2791.7         -85.958          39.809
v  Velocity[x]                  -4.546           4.508       0.0050662     -0.00026986
v  Velocity[y]                 -4.5766          4.5729        0.029219        0.053898
v  Velocity[z]             -1.6767e-06      2.2261e-06      2.1048e-10      1.5462e-12
v  Turb Kinetic Energy      6.4087e-10        0.079313      0.00025847      9.9041e-05
v  Turb Dissipation         1.8089e-07          7912.4           5.424         0.48557
v  Turb Viscosity           2.0316e-12         0.17624       0.0042085        0.025269
v  CFL                       0.0003513           221.3          11.581          3.6737
v  Fourier Number            0.0012602          21.974          1.4648          0.6296


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0055869          230.41          13.046          4.3033


 TIME FOR THE TIME STEP                9:        0.54825E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.8923E-11  0.1765E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2220E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COURANT MIN=  0.7973E-03 IN -0.1914E-01 -0.4471E-01  0.5000E-02

 FOURIER MAX=  0.2193E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1262E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2311E+03 IN  0.1577E-01  0.2762E-01  0.5000E-02
 COU/FOU MIN=  0.6515E-02 IN -0.2090E-01 -0.4383E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  7.9569e-07; norm:  8.0135e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.111630362E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884340E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 4.149693e-06, norm: 1.985879e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36435E+01 0.41972E+00
   Friction velocity        uet   :  0.10881E-02 0.32628E+00
   Friction velocity        uk    :  0.13940E-02 0.40731E+00
   Dimensionless distance   yplus :  0.35830E-01 0.12500E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1908
   Nb of faces within the viscous sub-layer     :       2297
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         10
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  7.9567e-07; norm:  8.0137e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.161712e-06, norm: 1.976671e+06, var: Var.  2
 velocity :     267848 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   238, res_abs :  1.9304e-09, res_nor :  9.9954e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.334773e-06, norm: 2.090455e+06, var: Var.  2
 velocity :     256538 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.6109E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.230286E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  7.9567e-07; norm:  8.0137e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.866916e-06, norm: 3.638384e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  7.9567e-07; norm:  8.0137e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.479380E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3058, res_abs :  2.2727e-09, res_nor :  9.8690e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.5324e-07; norm:  1.5671e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.886187E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2792, res_abs :  2.2654e-09, res_nor :  9.8374e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.0003e-06; norm:  1.5568e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.144214E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.5324e-07; norm:  1.5671e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.0003e-06; norm:  1.5568e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4316E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.285E-01 -0.119E-01  0.500E-02

 Max. velocity at interior face  0.4075E+01 ; min. -0.3938E+01
 Max. velocity at boundary face  0.4353E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415670E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.47938E-01    5850   0.62624E-02   0.20817E+00 
c  VelocityX    0.19313E+00     238   0.19038E+00   0.54232E+01 
c  VelocityY    0.19313E+00     238   0.19038E+00   0.56470E+01 
c  VelocityZ    0.19313E+00     238   0.19038E+00   0.10305E-13 
c  Turb Kinetic 0.99374E-03     145   0.20350E-03   0.94851E-04 
c  Turb Dissipa 0.67411E+02      84   0.29295E-04   0.39032E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy      -4.594e-06                             1
a  Turb Dissipation          -0.043583                            24


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4315.9          2709.5         -136.76          3.3257
v  Velocity[x]                 -3.7922          3.9328       0.0045664     -0.00032244
v  Velocity[y]                 -3.9012           4.153        0.027973        0.053922
v  Velocity[z]             -2.3707e-06      1.9629e-06      2.3605e-10      3.0071e-11
v  Turb Kinetic Energy      1.2019e-09        0.076307      0.00028673      0.00011134
v  Turb Dissipation         1.8331e-07            5732          5.2958         0.48509
v  Turb Viscosity           8.9228e-12          0.1765       0.0040118        0.023745
v  CFL                      0.00079732             222          11.563          3.6927
v  Fourier Number            0.0012616          21.927          1.4645          0.6072


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0065154          231.13          13.028          4.2999


 TIME FOR THE TIME STEP               10:        0.53878E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3568E-10  0.1766E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2312E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COURANT MIN=  0.1113E-02 IN -0.1726E-01 -0.4538E-01  0.5000E-02

 FOURIER MAX=  0.2194E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1263E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2403E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COU/FOU MIN=  0.6695E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.2456e-07; norm:  8.0026e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.102973498E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884330E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 4.329424e-06, norm: 2.040257e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34136E+01 0.42254E+00
   Friction velocity        uet   :  0.37558E-03 0.32714E+00
   Friction velocity        uk    :  0.15762E-02 0.40397E+00
   Dimensionless distance   yplus :  0.36389E-01 0.12701E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1793
   Nb of faces within the viscous sub-layer     :       2257
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         11
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.2454e-07; norm:  8.0028e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.347834e-06, norm: 2.028615e+06, var: Var.  2
 velocity :     270635 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   250, res_abs :  1.8553e-09, res_nor :  9.4738e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.467102e-06, norm: 2.151167e+06, var: Var.  2
 velocity :     259388 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5775E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.225714E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.2454e-07; norm:  8.0028e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.887174e-06, norm: 3.617781e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.2454e-07; norm:  8.0028e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.463707E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3059, res_abs :  2.2543e-09, res_nor :  9.9876e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.5063e-07; norm:  1.5755e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.901504E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2775, res_abs :  2.2449e-09, res_nor :  9.9456e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.0015e-06; norm:  1.5668e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.146604E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.5063e-07; norm:  1.5755e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.0015e-06; norm:  1.5668e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.3335E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.120E-01 -0.288E-01  0.500E-02

 Max. velocity at interior face  0.3876E+01 ; min. -0.3731E+01
 Max. velocity at boundary face  0.4353E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415669E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.46371E-01    5834   0.64951E-02   0.20544E+00 
c  VelocityX    0.19583E+00     250   0.17239E+00   0.55185E+01 
c  VelocityY    0.19583E+00     250   0.17239E+00   0.57769E+01 
c  VelocityZ    0.19583E+00     250   0.17239E+00   0.95404E-14 
c  Turb Kinetic 0.11015E-02     147   0.19329E-03   0.11443E-03 
c  Turb Dissipa 0.75217E+02      88   0.27330E-04   0.44387E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -4.2299e-07                             1
a  Turb Dissipation          -0.040919                            26


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -3335.2          2763.3         -171.15          -22.86
v  Velocity[x]                 -4.5201          4.4773       0.0039234     -0.00038539
v  Velocity[y]                 -4.5197           4.357        0.026788        0.053945
v  Velocity[z]             -2.4707e-06      4.3449e-07      2.4258e-10      5.0445e-11
v  Turb Kinetic Energy      7.1631e-10        0.081736      0.00034236      0.00012584
v  Turb Dissipation         1.8607e-07          6385.9          6.7872         0.57967
v  Turb Viscosity           3.5681e-11          0.1766       0.0038284        0.022288
v  CFL                        0.001113          231.18           11.61          3.7212
v  Fourier Number            0.0012632           21.94           1.466         0.58636


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0066948          240.31          13.076          4.3075


 TIME FOR THE TIME STEP               11:        0.55166E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3072E-10  0.1765E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2412E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COURANT MIN=  0.6443E-03 IN -0.1726E-01 -0.4538E-01  0.5000E-02

 FOURIER MAX=  0.2198E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1265E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2504E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COU/FOU MIN=  0.6798E-02 IN -0.1357E-01 -0.4673E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.5479e-07; norm:  8.0468e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.103672785E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884331E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 4.514380e-06, norm: 2.096273e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25385E+01 0.47040E+00
   Friction velocity        uet   :  0.68961E-03 0.32927E+00
   Friction velocity        uk    :  0.11675E-02 0.41904E+00
   Dimensionless distance   yplus :  0.52152E-01 0.12765E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1765
   Nb of faces within the viscous sub-layer     :       2187
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         12
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.5476e-07; norm:  8.0471e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.530372e-06, norm: 2.091549e+06, var: Var.  2
 velocity :     271815 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   264, res_abs :  1.9785e-09, res_nor :  9.9736e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.563286e-06, norm: 2.197043e+06, var: Var.  2
 velocity :     260424 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5789E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.222981E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.5476e-07; norm:  8.0471e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.870057e-06, norm: 3.585908e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.5476e-07; norm:  8.0471e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.432187E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3116, res_abs :  2.2142e-09, res_nor :  9.9302e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.3196e-07; norm:  1.5801e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.929197E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2774, res_abs :  2.2147e-09, res_nor :  9.9321e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.7840e-07; norm:  1.5769e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.150954E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.3196e-07; norm:  1.5801e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.7840e-07; norm:  1.5769e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.3169E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.649E-02 -0.260E-01  0.500E-02

 Max. velocity at interior face  0.3557E+01 ; min. -0.4088E+01
 Max. velocity at boundary face  0.4415E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415670E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@


 Write intermediate restart files
   checkpoint at iteration         12, Physical time    0.12000E-01


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

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

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

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


 Time for restart files:    0.20569E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.43219E-01    5890   0.67698E-02   0.19382E+00 
c  VelocityX    0.19837E+00     264   0.16101E+00   0.56911E+01 
c  VelocityY    0.19837E+00     264   0.16101E+00   0.60477E+01 
c  VelocityZ    0.19837E+00     264   0.16101E+00   0.10754E-13 
c  Turb Kinetic 0.12341E-02     146   0.21151E-03   0.81232E-04 
c  Turb Dissipa 0.85820E+02      86   0.19547E-04   0.28459E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -3.9572e-06                             1
a  Turb Dissipation          -0.037598                            24


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -3168.9          2878.2         -186.08         -33.313
v  Velocity[x]                 -3.8448          3.9528       0.0027229     -0.00043867
v  Velocity[y]                 -3.8728          4.0052        0.025841        0.053953
v  Velocity[z]             -2.3226e-06      3.4814e-07      2.2518e-10      6.3211e-11
v  Turb Kinetic Energy      9.5519e-10        0.061522      0.00037855      0.00014004
v  Turb Dissipation         1.8909e-07          4495.7          6.6803         0.59104
v  Turb Viscosity           3.0724e-11         0.17647       0.0036563        0.020891
v  CFL                      0.00064433          241.25          11.693          3.7541
v  Fourier Number             0.001265          21.981          1.4691         0.56687


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0067985          250.41          13.162           4.321


 TIME FOR THE TIME STEP               12:        0.58140E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.4678E-11  0.1761E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2438E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COURANT MIN=  0.5394E-03 IN -0.1726E-01 -0.4538E-01  0.5000E-02

 FOURIER MAX=  0.2197E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1267E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2530E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COU/FOU MIN=  0.5916E-02 IN -0.1357E-01 -0.4673E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.7664e-07; norm:  8.1659e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.161099356E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884330E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 4.610276e-06, norm: 2.147554e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26198E+01 0.53570E+00
   Friction velocity        uet   :  0.15751E-03 0.32225E+00
   Friction velocity        uk    :  0.13187E-02 0.41859E+00
   Dimensionless distance   yplus :  0.31197E-01 0.12971E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1688
   Nb of faces within the viscous sub-layer     :       2174
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         13
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.7661e-07; norm:  8.1661e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.607628e-06, norm: 2.149783e+06, var: Var.  2
 velocity :     273243 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   282, res_abs :  1.9663e-09, res_nor :  9.7915e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.499077e-06, norm: 2.273562e+06, var: Var.  2
 velocity :     262497 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4561E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.221346E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.7661e-07; norm:  8.1661e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.791294e-06, norm: 3.593041e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.7661e-07; norm:  8.1661e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.421398E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3114, res_abs :  2.1906e-09, res_nor :  9.8969e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.1334e-07; norm:  1.5735e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.918240E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2830, res_abs :  2.1982e-09, res_nor :  9.9309e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.4403e-07; norm:  1.5665e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.148340E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.1334e-07; norm:  1.5735e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.4403e-07; norm:  1.5665e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.3621E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.649E-02 -0.260E-01  0.500E-02

 Max. velocity at interior face  0.3721E+01 ; min. -0.4404E+01
 Max. velocity at boundary face  0.4487E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415639E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.42140E-01    5944   0.67017E-02   0.19038E+00 
c  VelocityX    0.20082E+00     282   0.14563E+00   0.60935E+01 
c  VelocityY    0.20082E+00     282   0.14563E+00   0.64935E+01 
c  VelocityZ    0.20082E+00     282   0.14563E+00   0.10743E-13 
c  Turb Kinetic 0.13644E-02     153   0.22774E-03   0.49144E-04 
c  Turb Dissipa 0.96052E+02      87   0.15284E-04   0.91663E+05 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -2.3999e-05                             3
a  Turb Dissipation           -0.17784                            21


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                      -3621          3018.8         -211.87         -52.152
v  Velocity[x]                 -3.9789          4.0106       0.0016148     -0.00050685
v  Velocity[y]                 -3.9316          3.8998        0.025195        0.053956
v  Velocity[z]             -2.6417e-06      2.0363e-06      2.0505e-10      7.1603e-11
v  Turb Kinetic Energy      1.0724e-09        0.065189      0.00043204      0.00015523
v  Turb Dissipation         1.9225e-07          4843.5          7.6295         0.66275
v  Turb Viscosity           4.6775e-12          0.1761       0.0034934        0.019564
v  CFL                      0.00053936           243.8           11.77          3.7836
v  Fourier Number            0.0012668          21.969           1.473         0.54842


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0059155          253.01          13.243          4.3321


 TIME FOR THE TIME STEP               13:        0.82291E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3487E-09  0.1755E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2380E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COURANT MIN=  0.1003E-02 IN -0.1726E-01 -0.4538E-01  0.5000E-02

 FOURIER MAX=  0.2173E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1269E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2473E+03 IN  0.1586E-01  0.2757E-01  0.5000E-02
 COU/FOU MIN=  0.5239E-02 IN -0.1357E-01 -0.4673E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.9010e-07; norm:  8.3121e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.366818221E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884361E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 4.550010e-06, norm: 2.223721e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28587E+01 0.61905E+00
   Friction velocity        uet   :  0.16946E-03 0.30065E+00
   Friction velocity        uk    :  0.10105E-02 0.42956E+00
   Dimensionless distance   yplus :  0.25406E-01 0.13090E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1618
   Nb of faces within the viscous sub-layer     :       2167
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         14
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.9007e-07; norm:  8.3124e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 4.537666e-06, norm: 2.230609e+06, var: Var.  2
 velocity :     274566 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   297, res_abs :  2.0273e-09, res_nor :  9.9605e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.822672e-06, norm: 2.346429e+06, var: Var.  2
 velocity :     263460 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5439E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.220350E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  8.9007e-07; norm:  8.3124e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 3.390946e-06, norm: 3.609382e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  8.9007e-07; norm:  8.3124e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.412788E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3045, res_abs :  2.1752e-09, res_nor :  9.8714e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.0495e-07; norm:  1.5566e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.900922E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2836, res_abs :  2.1992e-09, res_nor :  9.9805e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  9.2539e-07; norm:  1.5417e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.150590E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.0495e-07; norm:  1.5566e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.2539e-07; norm:  1.5417e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4303E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.649E-02 -0.260E-01  0.500E-02

 Max. velocity at interior face  0.3830E+01 ; min. -0.4517E+01
 Max. velocity at boundary face  0.4549E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415655E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.41279E-01    5881   0.68341E-02   0.18733E+00 
c  VelocityX    0.20354E+00     297   0.14822E+00   0.70272E+01 
c  VelocityY    0.20354E+00     297   0.14822E+00   0.73349E+01 
c  VelocityZ    0.20354E+00     297   0.14822E+00   0.19403E-13 
c  Turb Kinetic 0.14818E-02     156   0.30428E-03   0.83197E-04 
c  Turb Dissipa 0.10528E+03      88   0.11098E-03   0.33170E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -3.7987e-07                             2
a  Turb Dissipation          -0.035267                            21


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4302.9          3147.8         -245.81         -79.164
v  Velocity[x]                 -4.1264          4.1519      0.00082489     -0.00056455
v  Velocity[y]                 -4.0897          4.0332        0.025371        0.053966
v  Velocity[z]              -1.101e-06      5.8021e-07      1.8282e-10      7.6924e-11
v  Turb Kinetic Energy      1.4973e-09         0.11689      0.00049262       0.0001705
v  Turb Dissipation         1.9576e-07           11631          9.1634         0.76253
v  Turb Viscosity           3.4867e-10         0.17548       0.0033369        0.018317
v  CFL                        0.001003          238.01          11.827          3.8074
v  Fourier Number            0.0012688          21.734          1.4783         0.53076


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0052387          247.25          13.305          4.3381


 TIME FOR THE TIME STEP               14:        0.15119E+02

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1120E-09  0.1746E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2300E+03 IN  0.1595E-01  0.2752E-01  0.5000E-02
 COURANT MIN=  0.1147E-02 IN -0.1542E-01 -0.4605E-01  0.5000E-02

 FOURIER MAX=  0.2102E+02 IN -0.1134E-01 -0.3597E-01  0.5000E-02
 FOURIER MIN=  0.1271E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2393E+03 IN  0.1595E-01  0.2752E-01  0.5000E-02
 COU/FOU MIN=  0.5126E-02 IN  0.4014E-01 -0.2751E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.0102e-07; norm:  8.4243e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.140448907E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884345E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.902684e-06, norm: 2.285670e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30401E+01 0.70341E+00
   Friction velocity        uet   :  0.26618E-03 0.31176E+00
   Friction velocity        uk    :  0.95073E-03 0.43374E+00
   Dimensionless distance   yplus :  0.30077E-01 0.13208E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1557
   Nb of faces within the viscous sub-layer     :       2158
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         15
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.0098e-07; norm:  8.4247e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.894521e-06, norm: 2.289042e+06, var: Var.  2
 velocity :     275252 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   307, res_abs :  1.9857e-09, res_nor :  9.6436e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.088247e-06, norm: 2.407808e+06, var: Var.  2
 velocity :     264556 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4688E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.218871E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.0098e-07; norm:  8.4247e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.912779e-06, norm: 3.626977e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.0098e-07; norm:  8.4247e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.392634E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3077, res_abs :  2.1773e-09, res_nor :  9.9477e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.0478e-06; norm:  1.5242e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.877837E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2871, res_abs :  2.1844e-09, res_nor :  9.9802e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.0818e-06; norm:  1.5137e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.151870E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.0478e-06; norm:  1.5242e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.0818e-06; norm:  1.5137e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4789E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.669E-02 -0.262E-01  0.500E-02

 Max. velocity at interior face  0.4337E+01 ; min. -0.4649E+01
 Max. velocity at boundary face  0.4656E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415663E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.39263E-01    5948   0.69388E-02   0.17939E+00 
c  VelocityX    0.20591E+00     307   0.14413E+00   0.78809E+01 
c  VelocityY    0.20591E+00     307   0.14413E+00   0.82368E+01 
c  VelocityZ    0.20591E+00     307   0.14413E+00   0.30493E-14 
c  Turb Kinetic 0.15769E-02     164   0.30906E-03   0.78766E-04 
c  Turb Dissipa 0.11186E+03      94   0.72092E-04   0.30387E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -1.0876e-06                             2
a  Turb Dissipation           -0.03976                            17


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4788.7          3217.4         -284.84         -115.85
v  Velocity[x]                 -4.2715          4.7082      0.00059568     -0.00063664
v  Velocity[y]                 -4.3513          4.1909        0.025965        0.053963
v  Velocity[z]             -4.3434e-07      1.3808e-06      1.7043e-10      7.8716e-11
v  Turb Kinetic Energy      2.2097e-09        0.064821      0.00052898      0.00018379
v  Turb Dissipation         1.9959e-07          4385.4          8.7266         0.75592
v  Turb Viscosity           1.1196e-10         0.17458       0.0031862        0.017157
v  CFL                       0.0011473          230.03          11.845          3.8189
v  Fourier Number             0.001271          21.019          1.4833         0.51374


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.005126          239.28          13.328          4.3326


 TIME FOR THE TIME STEP               15:        0.14980E+02

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.9091E-11  0.1735E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.2114E+03 IN  0.1595E-01  0.2752E-01  0.5000E-02
 COURANT MIN=  0.1715E-02 IN -0.1542E-01 -0.4605E-01  0.5000E-02

 FOURIER MAX=  0.2214E+02 IN -0.1327E-01  0.1392E-01  0.5000E-02
 FOURIER MIN=  0.1273E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.2207E+03 IN  0.1595E-01  0.2752E-01  0.5000E-02
 COU/FOU MIN=  0.4559E-02 IN  0.4014E-01 -0.2751E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.0523e-07; norm:  8.4400e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.110889375E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884337E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 3.125664e-06, norm: 2.345955e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32676E+01 0.74509E+00
   Friction velocity        uet   :  0.58132E-04 0.41003E+00
   Friction velocity        uk    :  0.60272E-03 0.42245E+00
   Dimensionless distance   yplus :  0.59956E-02 0.13277E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1516
   Nb of faces within the viscous sub-layer     :       2129
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         16
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.0519e-07; norm:  8.4404e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 3.141097e-06, norm: 2.347277e+06, var: Var.  2
 velocity :     276061 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   311, res_abs :  2.0618e-09, res_nor :  9.8972e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.769859e-06, norm: 2.449989e+06, var: Var.  2
 velocity :     265350 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4510E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.216604E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.0519e-07; norm:  8.4404e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.685795e-06, norm: 3.609158e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.0519e-07; norm:  8.4404e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.386162E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3084, res_abs :  2.1518e-09, res_nor :  9.9342e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2303e-06; norm:  1.5236e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.905204E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2769, res_abs :  2.1330e-09, res_nor :  9.8474e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2976e-06; norm:  1.5204e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.153667E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2303e-06; norm:  1.5236e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2976e-06; norm:  1.5204e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4970E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.688E-02 -0.263E-01  0.500E-02

 Max. velocity at interior face  0.5360E+01 ; min. -0.4696E+01
 Max. velocity at boundary face  0.4749E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415637E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.38616E-01    5853   0.70944E-02   0.17828E+00 
c  VelocityX    0.20832E+00     311   0.13759E+00   0.85318E+01 
c  VelocityY    0.20832E+00     311   0.13759E+00   0.87768E+01 
c  VelocityZ    0.20832E+00     311   0.13759E+00   0.30878E-14 
c  Turb Kinetic 0.16577E-02     170   0.32176E-03   0.64933E-04 
c  Turb Dissipa 0.11550E+03     102   0.23737E-04   0.10845E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -1.5838e-06                             2
a  Turb Dissipation          -0.035707                            19


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4969.7          3260.1         -305.05         -142.51
v  Velocity[x]                 -4.4772          5.2615      0.00048687     -0.00069489
v  Velocity[y]                 -4.8104          4.4839        0.027111        0.053954
v  Velocity[z]             -1.0399e-06      2.3915e-06      1.9834e-10      7.5478e-11
v  Turb Kinetic Energy      2.9628e-09        0.096837      0.00058725      0.00019783
v  Turb Dissipation         2.0375e-07          6069.1          9.3708          0.8008
v  Turb Viscosity           9.0906e-12         0.17347       0.0030418        0.016085
v  CFL                       0.0017147          211.37          11.916          3.8258
v  Fourier Number            0.0012731          22.139          1.4904         0.49752


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0045594          220.65          13.406          4.3233


 TIME FOR THE TIME STEP               16:        0.58477E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1133E-10  0.1722E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1897E+03 IN  0.1603E-01  0.2747E-01  0.5000E-02
 COURANT MIN=  0.2435E-02 IN  0.3653E-01 -0.3218E-01  0.5000E-02

 FOURIER MAX=  0.2222E+02 IN -0.1313E-01  0.1405E-01  0.5000E-02
 FOURIER MIN=  0.1275E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1989E+03 IN  0.1603E-01  0.2747E-01  0.5000E-02
 COU/FOU MIN=  0.4170E-02 IN  0.4014E-01 -0.2751E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.2429e-07; norm:  8.3413e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.860996462E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884363E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.747058e-06, norm: 2.401745e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42078E+01 0.88929E+00
   Friction velocity        uet   :  0.32266E-04 0.48566E+00
   Friction velocity        uk    :  0.94095E-03 0.42953E+00
   Dimensionless distance   yplus :  0.59617E-01 0.13324E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1473
   Nb of faces within the viscous sub-layer     :       2144
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         17
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.2422e-07; norm:  8.3419e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.712604e-06, norm: 2.403963e+06, var: Var.  2
 velocity :     276282 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   308, res_abs :  2.0755e-09, res_nor :  9.8867e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.790608e-06, norm: 2.495882e+06, var: Var.  2
 velocity :     264923 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4545E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.213293E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.2422e-07; norm:  8.3419e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.668466e-06, norm: 3.613740e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.2422e-07; norm:  8.3419e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.378454E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3055, res_abs :  2.1113e-09, res_nor :  9.8985e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4530e-06; norm:  1.5446e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.899416E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2886, res_abs :  2.1116e-09, res_nor :  9.9000e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.5540e-06; norm:  1.5419e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.150010E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4530e-06; norm:  1.5446e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5540e-06; norm:  1.5419e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5007E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.121E-01 -0.289E-01  0.500E-02

 Max. velocity at interior face  0.5538E+01 ; min. -0.4896E+01
 Max. velocity at boundary face  0.4828E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415647E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37845E-01    5941   0.70331E-02   0.17743E+00 
c  VelocityX    0.20993E+00     308   0.13808E+00   0.88965E+01 
c  VelocityY    0.20993E+00     308   0.13808E+00   0.90302E+01 
c  VelocityZ    0.20993E+00     308   0.13808E+00   0.28929E-14 
c  Turb Kinetic 0.17209E-02     171   0.31151E-03   0.72699E-04 
c  Turb Dissipa 0.11739E+03     105   0.91926E-04   0.13290E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -1.9085e-06                             2
a  Turb Dissipation           -0.11572                            23


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5006.8          3287.5         -333.93          -176.1
v  Velocity[x]                  -4.777          5.2416      0.00067728     -0.00075749
v  Velocity[y]                 -5.1211          4.5552        0.028364        0.053946
v  Velocity[z]             -1.4995e-06      2.6106e-06      2.3891e-10       6.838e-11
v  Turb Kinetic Energy      3.6456e-09        0.087482      0.00064052      0.00021162
v  Turb Dissipation         2.0818e-07          5465.2          9.6398          0.8338
v  Turb Viscosity           1.1328e-11         0.17217       0.0029054        0.015096
v  CFL                       0.0024351          189.66          11.922          3.8113
v  Fourier Number            0.0012753          22.216          1.4981         0.48225


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0041699          198.95           13.42          4.2936


 TIME FOR THE TIME STEP               17:        0.58116E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.8699E-11  0.1707E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1693E+03 IN  0.1612E-01 -0.1043E-01  0.5000E-02
 COURANT MIN=  0.1336E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

 FOURIER MAX=  0.1825E+02 IN  0.1384E-01 -0.1335E-01  0.5000E-02
 FOURIER MIN=  0.1277E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1776E+03 IN  0.1612E-01 -0.1043E-01  0.5000E-02
 COU/FOU MIN=  0.3780E-02 IN  0.3888E-01 -0.2911E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.8700e-07; norm:  8.1356e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.193348305E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884353E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.782346e-06, norm: 2.462256e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42024E+01 0.95279E+00
   Friction velocity        uet   :  0.41364E-03 0.48901E+00
   Friction velocity        uk    :  0.12738E-02 0.46077E+00
   Dimensionless distance   yplus :  0.59106E-01 0.13309E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1453
   Nb of faces within the viscous sub-layer     :       2172
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         18
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.8691e-07; norm:  8.1363e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.776298e-06, norm: 2.473681e+06, var: Var.  2
 velocity :     276108 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   304, res_abs :  2.0304e-09, res_nor :  9.6363e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.981553e-06, norm: 2.564662e+06, var: Var.  2
 velocity :     264092 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4606E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.209273E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  9.8691e-07; norm:  8.1363e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.789307e-06, norm: 3.650408e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  9.8691e-07; norm:  8.1363e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.375787E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3060, res_abs :  2.0755e-09, res_nor :  9.9175e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4408e-06; norm:  1.5552e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.886546E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2841, res_abs :  2.0738e-09, res_nor :  9.9093e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.5268e-06; norm:  1.5528e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.140526E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4408e-06; norm:  1.5552e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5268e-06; norm:  1.5528e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4901E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.122E-01 -0.289E-01  0.500E-02

 Max. velocity at interior face  0.5434E+01 ; min. -0.4990E+01
 Max. velocity at boundary face  0.4890E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415651E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37579E-01    5901   0.67150E-02   0.17957E+00 
c  VelocityX    0.21071E+00     304   0.13404E+00   0.89075E+01 
c  VelocityY    0.21071E+00     304   0.13404E+00   0.88294E+01 
c  VelocityZ    0.21071E+00     304   0.13404E+00   0.18674E-14 
c  Turb Kinetic 0.17594E-02     168   0.21100E-03   0.76171E-04 
c  Turb Dissipa 0.12156E+03     101   0.53241E-04   0.15220E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -2.7386e-06                             3
a  Turb Dissipation          -0.043681                            28


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                      -4901          3392.8         -356.11         -197.44
v  Velocity[x]                 -5.0702          4.9225      0.00088876     -0.00078356
v  Velocity[y]                 -4.9866          5.0395        0.029483        0.053952
v  Velocity[z]             -1.4187e-06      1.9996e-06      3.1645e-10      6.0122e-11
v  Turb Kinetic Energy      4.1805e-09        0.095002      0.00069312      0.00022564
v  Turb Dissipation         2.1283e-07          6560.7          9.6432         0.85179
v  Turb Viscosity           8.6985e-12         0.17071       0.0027756         0.01419
v  CFL                       0.0013362          169.27          11.888          3.7776
v  Fourier Number            0.0012775           18.25          1.5057          0.4677


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0037799          177.62          13.393          4.2453


 TIME FOR THE TIME STEP               18:        0.58474E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1780E-09  0.1690E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1761E+03 IN  0.1612E-01 -0.1043E-01  0.5000E-02
 COURANT MIN=  0.7655E-03 IN  0.3770E-01 -0.3066E-01  0.5000E-02

 FOURIER MAX=  0.1830E+02 IN  0.1377E-01 -0.1342E-01  0.5000E-02
 FOURIER MIN=  0.1280E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1845E+03 IN  0.1612E-01 -0.1043E-01  0.5000E-02
 COU/FOU MIN=  0.3206E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1089e-06; norm:  7.8756e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.160876950E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884349E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.990974e-06, norm: 2.533159e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40276E+01 0.85795E+00
   Friction velocity        uet   :  0.38329E-03 0.47936E+00
   Friction velocity        uk    :  0.13941E-02 0.47153E+00
   Dimensionless distance   yplus :  0.66992E-01 0.13240E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1497
   Nb of faces within the viscous sub-layer     :       2146
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         19
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.1088e-06; norm:  7.8763e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.956836e-06, norm: 2.535330e+06, var: Var.  2
 velocity :     275720 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   302, res_abs :  2.1047e-09, res_nor :  9.9828e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.955968e-06, norm: 2.621431e+06, var: Var.  2
 velocity :     262342 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4576E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.204996E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.1088e-06; norm:  7.8763e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.832102e-06, norm: 3.677100e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1088e-06; norm:  7.8763e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.376994E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3157, res_abs :  2.0315e-09, res_nor :  9.9100e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2083e-06; norm:  1.5692e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.873973E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2848, res_abs :  2.0438e-09, res_nor :  9.9697e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2676e-06; norm:  1.5676e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.129017E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2083e-06; norm:  1.5692e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2676e-06; norm:  1.5676e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4813E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.122E-01 -0.289E-01  0.500E-02

 Max. velocity at interior face  0.5397E+01 ; min. -0.5126E+01
 Max. velocity at boundary face  0.4940E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415642E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37699E-01    6005   0.62937E-02   0.18390E+00 
c  VelocityX    0.21083E+00     302   0.12695E+00   0.86098E+01 
c  VelocityY    0.21083E+00     302   0.12695E+00   0.84601E+01 
c  VelocityZ    0.21083E+00     302   0.12695E+00   0.17146E-14 
c  Turb Kinetic 0.17702E-02     167   0.15837E-03   0.10659E-03 
c  Turb Dissipa 0.12546E+03     100   0.54476E-04   0.31549E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy      -1.963e-06                             4
a  Turb Dissipation          -0.053415                            28


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4813.3          3372.7         -370.25         -201.72
v  Velocity[x]                 -4.8487          4.3925       0.0010549     -0.00078454
v  Velocity[y]                 -4.7448          5.1528        0.030077        0.053983
v  Velocity[z]             -8.0539e-07      1.4272e-06      4.1235e-10      5.0936e-11
v  Turb Kinetic Energy      4.7294e-09         0.10245      0.00077731      0.00024279
v  Turb Dissipation         2.1765e-07          9024.1          10.657         0.93061
v  Turb Viscosity           1.7801e-10         0.16901       0.0026541        0.013353
v  CFL                      0.00076549           176.1           11.83          3.7286
v  Fourier Number            0.0012796          18.305          1.5172         0.45419


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0032059          184.52          13.347          4.1828


 TIME FOR THE TIME STEP               19:        0.59010E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.9812E-09  0.1671E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1812E+03 IN  0.1617E-01 -0.1034E-01  0.5000E-02
 COURANT MIN=  0.1450E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

 FOURIER MAX=  0.1861E+02 IN  0.1605E-01 -0.1059E-01  0.5000E-02
 FOURIER MIN=  0.1282E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1894E+03 IN  0.1617E-01 -0.1034E-01  0.5000E-02
 COU/FOU MIN=  0.3880E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2353e-06; norm:  7.6267e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.152482226E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884358E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.978621e-06, norm: 2.585211e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40962E+01 0.77760E+00
   Friction velocity        uet   :  0.28695E-03 0.48502E+00
   Friction velocity        uk    :  0.14856E-02 0.48129E+00
   Dimensionless distance   yplus :  0.46164E-01 0.13035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1492
   Nb of faces within the viscous sub-layer     :       2187
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         20
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.2352e-06; norm:  7.6270e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.995727e-06, norm: 2.580361e+06, var: Var.  2
 velocity :     273844 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   298, res_abs :  2.0318e-09, res_nor :  9.6388e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.753861e-06, norm: 2.660356e+06, var: Var.  2
 velocity :     261514 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4475E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.201191E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.2352e-06; norm:  7.6270e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.810871e-06, norm: 3.701285e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2352e-06; norm:  7.6270e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.374285E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3118, res_abs :  2.0081e-09, res_nor :  9.9813e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.0881e-06; norm:  1.5612e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.841992E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2842, res_abs :  1.9969e-09, res_nor :  9.9255e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1372e-06; norm:  1.5611e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.119228E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.0881e-06; norm:  1.5612e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1372e-06; norm:  1.5611e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4782E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.122E-01 -0.289E-01  0.500E-02

 Max. velocity at interior face  0.5151E+01 ; min. -0.4995E+01
 Max. velocity at boundary face  0.4966E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415640E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37429E-01    5960   0.59261E-02   0.18603E+00 
c  VelocityX    0.21079E+00     298   0.12215E+00   0.80387E+01 
c  VelocityY    0.21079E+00     298   0.12215E+00   0.79445E+01 
c  VelocityZ    0.21079E+00     298   0.12215E+00   0.44199E-14 
c  Turb Kinetic 0.17819E-02     171   0.16345E-03   0.14932E-03 
c  Turb Dissipa 0.12824E+03     103   0.23425E-04   0.35140E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -2.1907e-06                             3
a  Turb Dissipation          -0.049279                            24


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4782.4          3218.6         -397.29         -207.55
v  Velocity[x]                 -4.4688          4.3182       0.0010999     -0.00072622
v  Velocity[y]                 -4.3819          4.7335        0.030687        0.053993
v  Velocity[z]             -4.3196e-07      6.6036e-07      5.2219e-10      4.1137e-11
v  Turb Kinetic Energy      5.6498e-09        0.086621      0.00086014      0.00026036
v  Turb Dissipation         2.2259e-07          6770.3          10.519          0.9255
v  Turb Viscosity           9.8116e-10         0.16711       0.0025415         0.01259
v  CFL                       0.0014496          181.23          11.742          3.6647
v  Fourier Number            0.0012816           18.61          1.5316         0.44178


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.00388          189.42          13.274          4.1064


 TIME FOR THE TIME STEP               20:        0.57836E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3754E-09  0.1652E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1810E+03 IN  0.1617E-01 -0.1034E-01  0.5000E-02
 COURANT MIN=  0.2132E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

 FOURIER MAX=  0.1919E+02 IN -0.1881E-01  0.3758E-02  0.5000E-02
 FOURIER MIN=  0.1284E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1892E+03 IN  0.1617E-01 -0.1034E-01  0.5000E-02
 COU/FOU MIN=  0.4555E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3292e-06; norm:  7.4258e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.149756337E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884360E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.773395e-06, norm: 2.620042e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34281E+01 0.76102E+00
   Friction velocity        uet   :  0.43752E-03 0.44989E+00
   Friction velocity        uk    :  0.21072E-02 0.49256E+00
   Dimensionless distance   yplus :  0.23210E-01 0.12733E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1479
   Nb of faces within the viscous sub-layer     :       2198
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         21
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3290e-06; norm:  7.4272e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.778911e-06, norm: 2.620137e+06, var: Var.  2
 velocity :     272723 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   307, res_abs :  2.0647e-09, res_nor :  9.8063e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.508339e-06, norm: 2.708005e+06, var: Var.  2
 velocity :     261982 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4423E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.197668E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3290e-06; norm:  7.4272e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.767180e-06, norm: 3.731546e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3290e-06; norm:  7.4272e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.372170E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3179, res_abs :  1.9554e-09, res_nor :  9.8923e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.0763e-06; norm:  1.5306e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.830364E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2849, res_abs :  1.9578e-09, res_nor :  9.9044e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1280e-06; norm:  1.5291e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.116885E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.0763e-06; norm:  1.5306e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1280e-06; norm:  1.5291e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4766E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.803E-02 -0.278E-01  0.500E-02

 Max. velocity at interior face  0.4848E+01 ; min. -0.4594E+01
 Max. velocity at boundary face  0.4956E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415629E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37217E-01    6028   0.59132E-02   0.18828E+00 
c  VelocityX    0.21054E+00     307   0.11738E+00   0.73927E+01 
c  VelocityY    0.21054E+00     307   0.11738E+00   0.72969E+01 
c  VelocityZ    0.21054E+00     307   0.11738E+00   0.22774E-14 
c  Turb Kinetic 0.18292E-02     172   0.17109E-03   0.15699E-03 
c  Turb Dissipa 0.13060E+03     107   0.17850E-04   0.24603E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -2.4658e-06                             1
a  Turb Dissipation          -0.043182                            18


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4766.4          3023.7         -429.72         -216.89
v  Velocity[x]                 -4.2359          4.3208       0.0014975     -0.00066622
v  Velocity[y]                 -4.3416          4.3681        0.030818        0.053995
v  Velocity[z]             -1.2221e-07      1.8353e-07      6.0867e-10      3.0441e-11
v  Turb Kinetic Energy      7.8177e-09         0.11121       0.0009791      0.00028358
v  Turb Dissipation         2.2764e-07          5508.2          11.026         0.97262
v  Turb Viscosity           3.7535e-10         0.16522       0.0024353        0.011886
v  CFL                       0.0021324          180.98          11.628           3.587
v  Fourier Number            0.0012835          19.192          1.5535         0.43029


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0045546           189.2          13.181          4.0173


 TIME FOR THE TIME STEP               21:        0.58035E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3422E-10  0.1632E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1760E+03 IN  0.1617E-01 -0.1034E-01  0.5000E-02
 COURANT MIN=  0.2657E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

 FOURIER MAX=  0.2115E+02 IN -0.1881E-01  0.3758E-02  0.5000E-02
 FOURIER MIN=  0.1286E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1841E+03 IN  0.1617E-01 -0.1034E-01  0.5000E-02
 COU/FOU MIN=  0.5073E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3762e-06; norm:  7.2833e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813         0.132215851E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884371E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.508468e-06, norm: 2.669265e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28549E+01 0.72316E+00
   Friction velocity        uet   :  0.39249E-03 0.41496E+00
   Friction velocity        uk    :  0.13463E-02 0.50457E+00
   Dimensionless distance   yplus :  0.19343E-01 0.12224E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1468
   Nb of faces within the viscous sub-layer     :       2255
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         22
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3761e-06; norm:  7.2837e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.458573e-06, norm: 2.665439e+06, var: Var.  2
 velocity :     273784 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   322, res_abs :  2.0214e-09, res_nor :  9.6276e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.459107e-06, norm: 2.737502e+06, var: Var.  2
 velocity :     264459 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4387E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.193766E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3761e-06; norm:  7.2837e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.785214e-06, norm: 3.728523e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3761e-06; norm:  7.2837e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.375909E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3122, res_abs :  1.9172e-09, res_nor :  9.8946e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1654e-06; norm:  1.4784e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.844910E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2853, res_abs :  1.9308e-09, res_nor :  9.9648e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2313e-06; norm:  1.4733e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.124786E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1654e-06; norm:  1.4784e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2313e-06; norm:  1.4733e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4705E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.848E-02 -0.281E-01  0.500E-02

 Max. velocity at interior face  0.4471E+01 ; min. -0.4530E+01
 Max. velocity at boundary face  0.4936E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415645E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37591E-01    5975   0.64400E-02   0.19400E+00 
c  VelocityX    0.20996E+00     322   0.12097E+00   0.67216E+01 
c  VelocityY    0.20996E+00     322   0.12097E+00   0.66427E+01 
c  VelocityZ    0.20996E+00     322   0.12097E+00   0.14457E-14 
c  Turb Kinetic 0.19079E-02     173   0.23005E-03   0.19701E-03 
c  Turb Dissipa 0.13307E+03     106   0.18872E-04   0.28517E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -2.7738e-06                             3
a  Turb Dissipation          -0.047409                            16


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                      -4705          2801.2         -457.08         -222.86
v  Velocity[x]                 -4.1768          4.3349        0.001395     -0.00059348
v  Velocity[y]                 -4.3136          4.2916        0.031193        0.053996
v  Velocity[z]             -2.6314e-07       5.374e-07      6.8362e-10      1.9517e-11
v  Turb Kinetic Energy       1.057e-08         0.12792       0.0011204      0.00030991
v  Turb Dissipation         2.3282e-07          8228.6          11.952          1.0446
v  Turb Viscosity           3.4215e-11         0.16316       0.0023381         0.01124
v  CFL                       0.0026566          175.99          11.486          3.5022
v  Fourier Number            0.0012855          21.149          1.5815         0.41994


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0050727          184.15          13.068          3.9221


 TIME FOR THE TIME STEP               22:        0.58508E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1537E-09  0.1610E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1629E+03 IN  0.1623E-01 -0.1026E-01  0.5000E-02
 COURANT MIN=  0.2961E-02 IN  0.3655E-01 -0.3034E-01  0.5000E-02

 FOURIER MAX=  0.2222E+02 IN -0.1881E-01  0.3758E-02  0.5000E-02
 FOURIER MIN=  0.1288E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1710E+03 IN  0.1623E-01 -0.1026E-01  0.5000E-02
 COU/FOU MIN=  0.5403E-02 IN  0.3770E-01 -0.3066E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3842e-06; norm:  7.1844e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.740753325E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884355E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.488441e-06, norm: 2.703167e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28177E+01 0.87423E+00
   Friction velocity        uet   :  0.10298E-02 0.40271E+00
   Friction velocity        uk    :  0.22801E-02 0.51432E+00
   Dimensionless distance   yplus :  0.59115E-01 0.11651E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1462
   Nb of faces within the viscous sub-layer     :       2369
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         23
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3842e-06; norm:  7.1843e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.487973e-06, norm: 2.688360e+06, var: Var.  2
 velocity :     275134 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   335, res_abs :  2.0067e-09, res_nor :  9.6058e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.833077e-06, norm: 2.746398e+06, var: Var.  2
 velocity :     265073 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4383E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.189472E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3842e-06; norm:  7.1843e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.973387e-06, norm: 3.706308e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3842e-06; norm:  7.1843e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.381230E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3162, res_abs :  1.8683e-09, res_nor :  9.8605e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3656e-06; norm:  1.4191e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.866828E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2888, res_abs :  1.8912e-09, res_nor :  9.9813e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4642e-06; norm:  1.4110e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.134014E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3656e-06; norm:  1.4191e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4642e-06; norm:  1.4110e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4589E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.862E-02 -0.282E-01  0.500E-02

 Max. velocity at interior face  0.4460E+01 ; min. -0.4589E+01
 Max. velocity at boundary face  0.4914E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415659E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.38123E-01    6050   0.70730E-02   0.20121E+00 
c  VelocityX    0.20891E+00     335   0.11701E+00   0.60575E+01 
c  VelocityY    0.20891E+00     335   0.11701E+00   0.60058E+01 
c  VelocityZ    0.20891E+00     335   0.11701E+00   0.13962E-14 
c  Turb Kinetic 0.19955E-02     176   0.20084E-03   0.26049E-03 
c  Turb Dissipa 0.13423E+03     102   0.13683E-04   0.39275E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -2.0948e-06                             2
a  Turb Dissipation          -0.068995                            16


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4588.9          2521.3         -483.96         -230.65
v  Velocity[x]                 -4.0421          4.3587       0.0010088     -0.00052161
v  Velocity[y]                 -4.2032          4.2865        0.032195        0.053989
v  Velocity[z]             -4.2413e-07      5.7169e-07       7.289e-10      8.5285e-12
v  Turb Kinetic Energy      1.4759e-08          0.1379        0.001267      0.00033893
v  Turb Dissipation         2.3797e-07          8559.9          12.464          1.1064
v  Turb Viscosity           1.5372e-10           0.161       0.0022481        0.010645
v  CFL                        0.002961          162.87          11.344          3.4204
v  Fourier Number            0.0012875          22.216          1.6121         0.41057


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0054029          171.01          12.956           3.831


 TIME FOR THE TIME STEP               23:        0.59888E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1131E-08  0.1588E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1471E+03 IN  0.1623E-01 -0.1026E-01  0.5000E-02
 COURANT MIN=  0.3346E-02 IN  0.3655E-01 -0.3034E-01  0.5000E-02

 FOURIER MAX=  0.2394E+02 IN  0.1877E-01 -0.3955E-02  0.5000E-02
 FOURIER MIN=  0.1290E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1552E+03 IN  0.1623E-01 -0.1026E-01  0.5000E-02
 COU/FOU MIN=  0.6001E-02 IN -0.4018E-01 -0.2743E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3779e-06; norm:  7.0947e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.212683526E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884341E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.836877e-06, norm: 2.704687e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28445E+01 0.97912E+00
   Friction velocity        uet   :  0.51107E-03 0.40557E+00
   Friction velocity        uk    :  0.14830E-02 0.50215E+00
   Dimensionless distance   yplus :  0.64295E-01 0.11570E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1375
   Nb of faces within the viscous sub-layer     :       2396
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         24
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3780e-06; norm:  7.0943e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.694534e-06, norm: 2.692553e+06, var: Var.  2
 velocity :     275406 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   336, res_abs :  2.0120e-09, res_nor :  9.6851e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.797100e-06, norm: 2.737846e+06, var: Var.  2
 velocity :     265892 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4376E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.185122E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3780e-06; norm:  7.0943e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.945441e-06, norm: 3.665077e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3780e-06; norm:  7.0943e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.382971E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3166, res_abs :  1.8285e-09, res_nor :  9.8772e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7080e-06; norm:  1.3595e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.870904E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2895, res_abs :  1.8282e-09, res_nor :  9.8756e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.8245e-06; norm:  1.3511e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.135489E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7080e-06; norm:  1.3595e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8245e-06; norm:  1.3511e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4503E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.275E-01 -0.148E-01  0.500E-02

 Max. velocity at interior face  0.4195E+01 ; min. -0.4316E+01
 Max. velocity at boundary face  0.4874E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415654E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@


 Write intermediate restart files
   checkpoint at iteration         24, Physical time    0.24000E-01


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

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

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

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


 Time for restart files:    0.22136E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.38297E-01    6061   0.73189E-02   0.20688E+00 
c  VelocityX    0.20775E+00     336   0.11477E+00   0.54122E+01 
c  VelocityY    0.20775E+00     336   0.11477E+00   0.54467E+01 
c  VelocityZ    0.20775E+00     336   0.11477E+00   0.13987E-14 
c  Turb Kinetic 0.20986E-02     191   0.21534E-03   0.28588E-03 
c  Turb Dissipa 0.13619E+03     106   0.15039E-04   0.40356E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -3.5456e-06                             2
a  Turb Dissipation          -0.047735                            13


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4503.2          2266.2         -505.97         -235.26
v  Velocity[x]                 -3.9994          4.3635      0.00040829     -0.00045318
v  Velocity[y]                 -4.1465          4.1785        0.033512        0.054007
v  Velocity[z]             -4.4883e-07      6.5382e-07      7.4142e-10     -1.3846e-12
v  Turb Kinetic Energy      2.6477e-08         0.14748       0.0014319      0.00037163
v  Turb Dissipation         2.4344e-07          7089.6          13.048          1.1825
v  Turb Viscosity           1.1305e-09         0.15879       0.0021648        0.010097
v  CFL                       0.0033462          147.08          11.202          3.3452
v  Fourier Number            0.0012897          23.942          1.6442         0.40193


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0060009           155.2          12.846          3.7471


 TIME FOR THE TIME STEP               24:        0.62724E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1235E-08  0.1567E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1313E+03 IN  0.1623E-01 -0.1026E-01  0.5000E-02
 COURANT MIN=  0.2757E-02 IN -0.1207E-01 -0.4310E-01  0.5000E-02

 FOURIER MAX=  0.2836E+02 IN  0.1725E-01 -0.8499E-02  0.5000E-02
 FOURIER MIN=  0.1292E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1395E+03 IN -0.2970E-01  0.1139E-01  0.5000E-02
 COU/FOU MIN=  0.5524E-02 IN -0.4018E-01 -0.2743E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3690e-06; norm:  6.9972e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.136303763E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884346E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.789631e-06, norm: 2.693666e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24504E+01 0.10094E+01
   Friction velocity        uet   :  0.35579E-03 0.38417E+00
   Friction velocity        uk    :  0.20300E-02 0.49074E+00
   Dimensionless distance   yplus :  0.73455E-01 0.11480E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1336
   Nb of faces within the viscous sub-layer     :       2453
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         25
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3689e-06; norm:  6.9979e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.858170e-06, norm: 2.686258e+06, var: Var.  2
 velocity :     276082 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   342, res_abs :  2.0287e-09, res_nor :  9.8134e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.767301e-06, norm: 2.728610e+06, var: Var.  2
 velocity :     266012 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4486E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.180986E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3689e-06; norm:  6.9979e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.896413e-06, norm: 3.626245e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3689e-06; norm:  6.9979e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.369740E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3156, res_abs :  1.8055e-09, res_nor :  9.9758e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.8142e-06; norm:  1.3035e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.851909E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2885, res_abs :  1.8092e-09, res_nor :  9.9963e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.9422e-06; norm:  1.2981e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.127233E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8142e-06; norm:  1.3035e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.9422e-06; norm:  1.2981e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4519E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.276E-01 -0.148E-01  0.500E-02

 Max. velocity at interior face  0.4385E+01 ; min. -0.4259E+01
 Max. velocity at boundary face  0.4808E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415647E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.36974E-01    6041   0.70300E-02   0.20429E+00 
c  VelocityX    0.20672E+00     342   0.10449E+00   0.48960E+01 
c  VelocityY    0.20672E+00     342   0.10449E+00   0.50055E+01 
c  VelocityZ    0.20672E+00     342   0.10449E+00   0.13291E-14 
c  Turb Kinetic 0.21764E-02     206   0.26717E-03   0.30946E-03 
c  Turb Dissipa 0.13611E+03     118   0.21514E-04   0.38783E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -1.6961e-06                             2
a  Turb Dissipation          -0.075604                            15


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4518.6          2163.2         -537.34         -250.44
v  Velocity[x]                 -3.9906          4.3606     -0.00027952      -0.0003978
v  Velocity[y]                 -4.1315          4.0732        0.034557        0.054011
v  Velocity[z]             -4.3493e-07      6.6022e-07      7.2755e-10      -9.761e-12
v  Turb Kinetic Energy      4.6239e-08         0.15288       0.0016029      0.00040559
v  Turb Dissipation         2.4939e-07          4879.7          13.158          1.1998
v  Turb Viscosity           1.2355e-09         0.15666        0.002086       0.0095871
v  CFL                       0.0027574          131.26          11.055          3.2781
v  Fourier Number             0.001292          28.364          1.6834         0.39408


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0055239          139.49          12.739          3.6722


 TIME FOR THE TIME STEP               25:        0.60904E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.7571E-09  0.1545E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1331E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COURANT MIN=  0.2159E-02 IN -0.1207E-01 -0.4310E-01  0.5000E-02

 FOURIER MAX=  0.3422E+02 IN  0.1725E-01 -0.8499E-02  0.5000E-02
 FOURIER MIN=  0.1295E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1439E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COU/FOU MIN=  0.5437E-02 IN -0.4119E-01 -0.2572E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4144e-06; norm:  6.8884e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.146442876E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884353E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.786966e-06, norm: 2.678970e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22585E+01 0.99763E+00
   Friction velocity        uet   :  0.74527E-06 0.37574E+00
   Friction velocity        uk    :  0.17743E-02 0.46348E+00
   Dimensionless distance   yplus :  0.32223E-01 0.11359E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1285
   Nb of faces within the viscous sub-layer     :       2462
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         26
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4145e-06; norm:  6.8881e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.828917e-06, norm: 2.674701e+06, var: Var.  2
 velocity :     276189 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   348, res_abs :  1.9638e-09, res_nor :  9.5472e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.650698e-06, norm: 2.720669e+06, var: Var.  2
 velocity :     265056 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4672E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.176736E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4145e-06; norm:  6.8881e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.757726e-06, norm: 3.588460e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4145e-06; norm:  6.8881e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.358797E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3107, res_abs :  1.7634e-09, res_nor :  9.9775e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6185e-06; norm:  1.2455e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.816624E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2853, res_abs :  1.7539e-09, res_nor :  9.9236e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7309e-06; norm:  1.2444e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.118555E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6185e-06; norm:  1.2455e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7309e-06; norm:  1.2444e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4559E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.276E-01 -0.145E-01  0.500E-02

 Max. velocity at interior face  0.4458E+01 ; min. -0.4326E+01
 Max. velocity at boundary face  0.4727E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415642E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.35880E-01    5960   0.67080E-02   0.20301E+00 
c  VelocityX    0.20569E+00     348   0.97054E-01   0.44816E+01 
c  VelocityY    0.20569E+00     348   0.97054E-01   0.46144E+01 
c  VelocityZ    0.20569E+00     348   0.97054E-01   0.11670E-14 
c  Turb Kinetic 0.22482E-02     217   0.34049E-03   0.34864E-03 
c  Turb Dissipa 0.13658E+03     134   0.31306E-04   0.49219E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -1.3063e-06                             2
a  Turb Dissipation          -0.094055                            12


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4558.8          2034.8         -563.73         -261.94
v  Velocity[x]                 -4.2066          4.3414     -0.00053303     -0.00036422
v  Velocity[y]                 -4.1901          4.0309        0.035392         0.05399
v  Velocity[z]             -3.5541e-07      6.0609e-07       6.938e-10     -1.6136e-11
v  Turb Kinetic Energy      4.9113e-08          0.1538       0.0018016      0.00044363
v  Turb Dissipation         2.5592e-07          8546.7          13.655          1.2516
v  Turb Viscosity           7.5712e-10         0.15446       0.0020122       0.0091118
v  CFL                       0.0021592          133.06          10.968          3.2243
v  Fourier Number            0.0012945          34.217          1.7345         0.38712


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0054373          143.92          12.702          3.6114


 TIME FOR THE TIME STEP               26:        0.62403E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3885E-08  0.1522E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1414E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COURANT MIN=  0.2186E-02 IN -0.1107E-01 -0.4425E-01  0.5000E-02

 FOURIER MAX=  0.3911E+02 IN  0.1677E-01 -0.9309E-02  0.5000E-02
 FOURIER MIN=  0.1297E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1525E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COU/FOU MIN=  0.4320E-02 IN -0.4219E-01 -0.2404E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4873e-06; norm:  6.7699e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.109996789E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884358E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.644601e-06, norm: 2.674629e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23611E+01 0.98016E+00
   Friction velocity        uet   :  0.67915E-03 0.38617E+00
   Friction velocity        uk    :  0.19901E-02 0.49111E+00
   Dimensionless distance   yplus :  0.29250E-01 0.11509E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1241
   Nb of faces within the viscous sub-layer     :       2404
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         27
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4874e-06; norm:  6.7694e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.640633e-06, norm: 2.682609e+06, var: Var.  2
 velocity :     275462 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   355, res_abs :  2.0334e-09, res_nor :  9.9329e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.540977e-06, norm: 2.727383e+06, var: Var.  2
 velocity :     265224 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4782E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.171860E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4874e-06; norm:  6.7694e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.629351e-06, norm: 3.558870e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4874e-06; norm:  6.7694e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.346845E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3125, res_abs :  1.7110e-09, res_nor :  9.9561e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4302e-06; norm:  1.1986e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.781187E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2848, res_abs :  1.7112e-09, res_nor :  9.9572e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.5342e-06; norm:  1.1994e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.112719E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4302e-06; norm:  1.1986e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5342e-06; norm:  1.1994e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4667E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.273E-01 -0.146E-01  0.500E-02

 Max. velocity at interior face  0.4476E+01 ; min. -0.4352E+01
 Max. velocity at boundary face  0.4656E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415647E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.34685E-01    5973   0.65587E-02   0.20182E+00 
c  VelocityX    0.20471E+00     355   0.90671E-01   0.40803E+01 
c  VelocityY    0.20471E+00     355   0.90671E-01   0.42876E+01 
c  VelocityZ    0.20471E+00     355   0.90671E-01   0.10881E-14 
c  Turb Kinetic 0.23281E-02     228   0.50542E-03   0.42466E-03 
c  Turb Dissipa 0.13938E+03     138   0.24226E-04   0.52406E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy     -1.0459e-06                             2
a  Turb Dissipation          -0.010141                             9


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                      -4667          1863.9         -590.02         -275.08
v  Velocity[x]                 -4.2518          4.2967     -0.00086821     -0.00035102
v  Velocity[y]                 -4.3252          4.0918        0.036041         0.05397
v  Velocity[z]             -1.7342e-07      4.7426e-07      6.3677e-10     -2.2255e-11
v  Turb Kinetic Energy      5.0042e-08         0.15642       0.0020149      0.00048419
v  Turb Dissipation         2.6316e-07          9397.5          13.551           1.282
v  Turb Viscosity            3.885e-09         0.15225       0.0019428       0.0086675
v  CFL                       0.0021858          141.45           10.93          3.1843
v  Fourier Number            0.0012973          39.109           1.796         0.38097


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0043205          152.45          12.726          3.5653


 TIME FOR THE TIME STEP               27:        0.60477E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1217E-08  0.1501E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1454E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COURANT MIN=  0.1725E-02 IN -0.1107E-01 -0.4425E-01  0.5000E-02

 FOURIER MAX=  0.4607E+02 IN  0.1916E-01  0.8455E-03  0.5000E-02
 FOURIER MIN=  0.1300E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1566E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COU/FOU MIN=  0.3726E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5489e-06; norm:  6.6453e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.561805092E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884353E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.511403e-06, norm: 2.688784e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24847E+01 0.11978E+01
   Friction velocity        uet   :  0.61011E-03 0.39447E+00
   Friction velocity        uk    :  0.12858E-02 0.48776E+00
   Dimensionless distance   yplus :  0.13963E-01 0.11639E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1226
   Nb of faces within the viscous sub-layer     :       2349
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         28
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.5491e-06; norm:  6.6445e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.512884e-06, norm: 2.685960e+06, var: Var.  2
 velocity :     275362 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   368, res_abs :  1.9739e-09, res_nor :  9.6792e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.500995e-06, norm: 2.703722e+06, var: Var.  2
 velocity :     264550 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4844E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.166355E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.5491e-06; norm:  6.6445e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.513840e-06, norm: 3.506969e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5491e-06; norm:  6.6445e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.341281E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3144, res_abs :  1.6425e-09, res_nor :  9.8737e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4982e-06; norm:  1.1634e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.732239E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2843, res_abs :  1.6578e-09, res_nor :  9.9653e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6317e-06; norm:  1.1631e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.106588E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4982e-06; norm:  1.1634e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6317e-06; norm:  1.1631e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4815E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.269E-01 -0.154E-01  0.500E-02

 Max. velocity at interior face  0.4545E+01 ; min. -0.4378E+01
 Max. velocity at boundary face  0.4574E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415647E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.34128E-01    5987   0.64073E-02   0.20515E+00 
c  VelocityX    0.20393E+00     368   0.85537E-01   0.36969E+01 
c  VelocityY    0.20393E+00     368   0.85537E-01   0.40098E+01 
c  VelocityZ    0.20393E+00     368   0.85537E-01   0.10255E-14 
c  Turb Kinetic 0.24059E-02     239   0.61676E-03   0.48285E-03 
c  Turb Dissipa 0.14118E+03     145   0.23938E-04   0.42410E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation           -0.13082                             6


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4814.5          1795.4         -612.47          -287.9
v  Velocity[x]                 -4.1667          4.2647     -0.00088809     -0.00034352
v  Velocity[y]                 -4.2763          4.1118        0.036676        0.053961
v  Velocity[z]             -1.0884e-07      2.8762e-07      5.6574e-10     -2.7572e-11
v  Turb Kinetic Energy      4.0104e-08         0.18412        0.002275      0.00052758
v  Turb Dissipation         2.6946e-07          8825.7          13.789           1.338
v  Turb Viscosity           1.2173e-09         0.15006       0.0018787       0.0082485
v  CFL                       0.0017252          145.43          10.895          3.1531
v  Fourier Number            0.0013002          46.069          1.8811         0.37621


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0037263          156.63          12.776          3.5293


 TIME FOR THE TIME STEP               28:        0.60666E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.7569E-09  0.1479E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1478E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COURANT MIN=  0.9471E-03 IN -0.9790E-02 -0.4643E-01  0.5000E-02

 FOURIER MAX=  0.5437E+02 IN  0.1916E-01  0.8455E-03  0.5000E-02
 FOURIER MIN=  0.1303E-02 IN  0.1457E-01  0.4623E-01  0.5000E-02

 COU/FOU MAX=  0.1592E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COU/FOU MIN=  0.2557E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6385e-06; norm:  6.5263e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.155229604E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884353E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.453701e-06, norm: 2.670702e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25273E+01 0.13807E+01
   Friction velocity        uet   :  0.42702E-03 0.39079E+00
   Friction velocity        uk    :  0.16837E-02 0.50542E+00
   Dimensionless distance   yplus :  0.41033E-01 0.11756E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1193
   Nb of faces within the viscous sub-layer     :       2385
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         29
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.6384e-06; norm:  6.5265e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.331238e-06, norm: 2.671246e+06, var: Var.  2
 velocity :     273429 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   378, res_abs :  1.9831e-09, res_nor :  9.7536e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.287937e-06, norm: 2.665151e+06, var: Var.  2
 velocity :     262630 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4919E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.160956E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.6384e-06; norm:  6.5265e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.315977e-06, norm: 3.449625e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6384e-06; norm:  6.5265e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.333096E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3124, res_abs :  1.6041e-09, res_nor :  9.9660e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3468e-06; norm:  1.1297e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.706195E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2749, res_abs :  1.6085e-09, res_nor :  9.9935e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4612e-06; norm:  1.1283e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.102680E-02, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3468e-06; norm:  1.1297e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4612e-06; norm:  1.1283e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4986E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.269E-01 -0.155E-01  0.500E-02

 Max. velocity at interior face  0.4606E+01 ; min. -0.4445E+01
 Max. velocity at boundary face  0.4474E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415645E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.33310E-01    5873   0.63794E-02   0.20695E+00 
c  VelocityX    0.20332E+00     378   0.82026E-01   0.33911E+01 
c  VelocityY    0.20332E+00     378   0.82026E-01   0.37535E+01 
c  VelocityZ    0.20332E+00     378   0.82026E-01   0.92125E-15 
c  Turb Kinetic 0.24635E-02     247   0.76968E-03   0.52718E-03 
c  Turb Dissipa 0.14005E+03     145   0.27129E-04   0.29581E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation         -0.0091466                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4986.2          1861.4         -628.62         -299.96
v  Velocity[x]                 -4.1249          4.3034     -0.00018576     -0.00035107
v  Velocity[y]                 -4.1234           4.002        0.037354        0.053974
v  Velocity[z]             -9.6705e-08      3.4715e-07      4.9084e-10     -3.2768e-11
v  Turb Kinetic Energy      3.9664e-08         0.20683       0.0025434      0.00056955
v  Turb Dissipation         2.7516e-07          5730.4          13.557          1.3175
v  Turb Viscosity           7.5693e-10         0.14787       0.0018176        0.007849
v  CFL                      0.00094714          147.75          10.847          3.1284
v  Fourier Number            0.0013034           54.37          1.9749           0.372


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0025571          159.17          12.822          3.5004


 TIME FOR THE TIME STEP               29:        0.60772E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.7545E-09  0.1456E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1502E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COURANT MIN=  0.2113E-03 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.6708E+02 IN -0.1883E-01  0.3659E-02  0.5000E-02
 FOURIER MIN=  0.1304E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1619E+03 IN  0.1148E-01  0.2966E-01  0.5000E-02
 COU/FOU MIN=  0.1743E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7118e-06; norm:  6.4371e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.170356446E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884355E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.276182e-06, norm: 2.634067e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23423E+01 0.13785E+01
   Friction velocity        uet   :  0.62841E-04 0.37903E+00
   Friction velocity        uk    :  0.13401E-02 0.49454E+00
   Dimensionless distance   yplus :  0.42336E-01 0.11875E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1157
   Nb of faces within the viscous sub-layer     :       2382
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         30
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.7119e-06; norm:  6.4364e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.292559e-06, norm: 2.627379e+06, var: Var.  2
 velocity :     271992 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   382, res_abs :  1.9890e-09, res_nor :  9.8014e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.264210e-06, norm: 2.614016e+06, var: Var.  2
 velocity :     260863 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4993E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.156220E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.7119e-06; norm:  6.4364e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.218093e-06, norm: 3.369824e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7119e-06; norm:  6.4364e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.324831E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3178, res_abs :  1.5528e-09, res_nor :  9.9398e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3704e-06; norm:  1.0923e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.692998E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2874, res_abs :  1.5416e-09, res_nor :  9.8680e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4708e-06; norm:  1.0918e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.971576E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3704e-06; norm:  1.0923e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4708e-06; norm:  1.0918e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5135E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.270E-01 -0.158E-01  0.500E-02

 Max. velocity at interior face  0.4612E+01 ; min. -0.4483E+01
 Max. velocity at boundary face  0.4441E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415650E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.32483E-01    6052   0.62193E-02   0.20793E+00 
c  VelocityX    0.20293E+00     382   0.81894E-01   0.31746E+01 
c  VelocityY    0.20293E+00     382   0.81894E-01   0.34453E+01 
c  VelocityZ    0.20293E+00     382   0.81894E-01   0.77862E-15 
c  Turb Kinetic 0.24882E-02     249   0.89897E-03   0.55666E-03 
c  Turb Dissipa 0.13475E+03     143   0.22928E-04   0.20969E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation         -0.0066093                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5135.2          1963.1         -649.72         -321.08
v  Velocity[x]                 -4.2817          4.3144       0.0015001     -0.00036088
v  Velocity[y]                 -4.2668          4.0948        0.038717        0.053969
v  Velocity[z]             -8.7264e-08      4.9725e-07      4.2044e-10     -3.6847e-11
v  Turb Kinetic Energy      2.2567e-08         0.20905       0.0028433      0.00061431
v  Turb Dissipation         2.8124e-07          7038.5          13.299          1.3136
v  Turb Viscosity           7.5451e-10         0.14558       0.0017677       0.0074774
v  CFL                      0.00021131          150.18          10.773           3.106
v  Fourier Number            0.0013042          67.081          2.0909         0.36969


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017426          161.85          12.864          3.4757


 TIME FOR THE TIME STEP               30:        0.61875E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.4966E-09  0.1434E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1497E+03 IN  0.1157E-01  0.2963E-01  0.5000E-02
 COURANT MIN=  0.2130E-03 IN -0.7835E-02 -0.4791E-01  0.5000E-02

 FOURIER MAX=  0.8964E+02 IN -0.1881E-01  0.3758E-02  0.5000E-02
 FOURIER MIN=  0.1304E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1609E+03 IN  0.1157E-01  0.2963E-01  0.5000E-02
 COU/FOU MIN=  0.1738E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7890e-06; norm:  6.3870e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813         0.113158599E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884350E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.269007e-06, norm: 2.583086e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21056E+01 0.12725E+01
   Friction velocity        uet   :  0.27738E-03 0.35865E+00
   Friction velocity        uk    :  0.12206E-02 0.47720E+00
   Dimensionless distance   yplus :  0.21997E-01 0.11940E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1127
   Nb of faces within the viscous sub-layer     :       2407
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         31
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.7892e-06; norm:  6.3859e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.279352e-06, norm: 2.579075e+06, var: Var.  2
 velocity :     270463 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   382, res_abs :  2.0122e-09, res_nor :  9.9219e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.284658e-06, norm: 2.562956e+06, var: Var.  2
 velocity :     258492 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5074E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.151981E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.7892e-06; norm:  6.3859e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.206327e-06, norm: 3.313737e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7892e-06; norm:  6.3859e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.314183E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3176, res_abs :  1.4921e-09, res_nor :  9.8176e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.5924e-06; norm:  1.0240e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.674744E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2870, res_abs :  1.5194e-09, res_nor :  9.9975e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6919e-06; norm:  1.0238e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.930535E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5924e-06; norm:  1.0240e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6919e-06; norm:  1.0238e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5204E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.271E-01 -0.156E-01  0.500E-02

 Max. velocity at interior face  0.4374E+01 ; min. -0.4595E+01
 Max. velocity at boundary face  0.4399E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415650E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.31418E-01    6046   0.61227E-02   0.20673E+00 
c  VelocityX    0.20280E+00     382   0.81026E-01   0.30934E+01 
c  VelocityY    0.20280E+00     382   0.81026E-01   0.32165E+01 
c  VelocityZ    0.20280E+00     382   0.81026E-01   0.65708E-15 
c  Turb Kinetic 0.24944E-02     244   0.11704E-02   0.61704E-03 
c  Turb Dissipa 0.12825E+03     141   0.42319E-04   0.17060E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.013726                             6


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5204.2          2048.3         -669.22         -339.46
v  Velocity[x]                 -4.4121          4.4079       0.0038319     -0.00044116
v  Velocity[y]                 -4.3624          4.1926        0.041126        0.053973
v  Velocity[z]              -7.881e-08      4.8501e-07      3.5188e-10     -3.9993e-11
v  Turb Kinetic Energy      5.5993e-08         0.18966       0.0031682       0.0006629
v  Turb Dissipation         2.8773e-07          5775.6          13.041           1.321
v  Turb Viscosity            4.966e-10         0.14336       0.0017274       0.0071293
v  CFL                      0.00021299          149.67          10.691          3.0856
v  Fourier Number            0.0013043          89.642          2.2202         0.36881


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017384          160.92          12.911          3.4545


 TIME FOR THE TIME STEP               31:        0.61510E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3009E-08  0.1411E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1476E+03 IN  0.1157E-01  0.2963E-01  0.5000E-02
 COURANT MIN=  0.2523E-03 IN -0.6851E-02 -0.4587E-01  0.5000E-02

 FOURIER MAX=  0.9792E+02 IN -0.1879E-01  0.3857E-02  0.5000E-02
 FOURIER MIN=  0.1305E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1590E+03 IN  0.1157E-01  0.2963E-01  0.5000E-02
 COU/FOU MIN=  0.1934E-02 IN -0.3885E-02 -0.4839E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8992e-06; norm:  6.3660e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813         0.243672845E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884350E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.260830e-06, norm: 2.539728e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22480E+01 0.10711E+01
   Friction velocity        uet   :  0.71682E-04 0.36693E+00
   Friction velocity        uk    :  0.13670E-02 0.45964E+00
   Dimensionless distance   yplus :  0.53642E-01 0.12009E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1104
   Nb of faces within the viscous sub-layer     :       2384
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         32
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.8994e-06; norm:  6.3652e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.261537e-06, norm: 2.531653e+06, var: Var.  2
 velocity :     268085 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   393, res_abs :  1.9457e-09, res_nor :  9.5949e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.201565e-06, norm: 2.512590e+06, var: Var.  2
 velocity :     256418 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5115E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.148318E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.8994e-06; norm:  6.3652e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.205712e-06, norm: 3.260499e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8994e-06; norm:  6.3652e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.297757E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3152, res_abs :  1.4765e-09, res_nor :  9.9549e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3085e-06; norm:  9.5542e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.643727E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2786, res_abs :  1.4625e-09, res_nor :  9.8607e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3604e-06; norm:  9.5398e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.904548E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3085e-06; norm:  9.5542e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3604e-06; norm:  9.5398e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5191E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.272E-01 -0.155E-01  0.500E-02

 Max. velocity at interior face  0.4307E+01 ; min. -0.4545E+01
 Max. velocity at boundary face  0.4347E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415641E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.29776E-01    5938   0.60987E-02   0.20076E+00 
c  VelocityX    0.20279E+00     393   0.83198E-01   0.30464E+01 
c  VelocityY    0.20279E+00     393   0.83198E-01   0.30865E+01 
c  VelocityZ    0.20279E+00     393   0.83198E-01   0.63332E-15 
c  Turb Kinetic 0.25150E-02     233   0.12969E-02   0.69041E-03 
c  Turb Dissipa 0.12124E+03     137   0.71656E-04   0.35314E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.063931                             8


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5190.9          2103.2         -690.07         -357.58
v  Velocity[x]                 -4.4723          4.5031       0.0055555     -0.00057884
v  Velocity[y]                 -4.4157          4.3935        0.043022        0.053993
v  Velocity[z]             -7.2506e-08        3.36e-07      2.8235e-10       -4.18e-11
v  Turb Kinetic Energy      7.0967e-08         0.18954       0.0034999      0.00071373
v  Turb Dissipation         2.9447e-07          8965.2          13.782          1.3795
v  Turb Viscosity            3.009e-09         0.14112       0.0016927        0.006797
v  CFL                       0.0002523          147.55           10.58          3.0644
v  Fourier Number            0.0013045           97.92          2.3536         0.36869


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0019341          159.02          12.934          3.4331


 TIME FOR THE TIME STEP               32:        0.63264E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3865E-08  0.1387E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1427E+03 IN  0.1167E-01  0.2959E-01  0.5000E-02
 COURANT MIN=  0.3294E-03 IN -0.4144E-02 -0.4530E-01  0.5000E-02

 FOURIER MAX=  0.1009E+03 IN  0.9611E-02 -0.3032E-01  0.5000E-02
 FOURIER MIN=  0.1305E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1538E+03 IN  0.1157E-01  0.2963E-01  0.5000E-02
 COU/FOU MIN=  0.2268E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.9765e-06; norm:  6.3460e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.159965609E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884359E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.214962e-06, norm: 2.493079e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21849E+01 0.10078E+01
   Friction velocity        uet   :  0.26078E-03 0.36386E+00
   Friction velocity        uk    :  0.12325E-02 0.47134E+00
   Dimensionless distance   yplus :  0.36737E-01 0.12042E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1066
   Nb of faces within the viscous sub-layer     :       2407
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         33
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.9766e-06; norm:  6.3458e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.246221e-06, norm: 2.489005e+06, var: Var.  2
 velocity :     265296 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   390, res_abs :  1.9554e-09, res_nor :  9.6505e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.206355e-06, norm: 2.474919e+06, var: Var.  2
 velocity :     254397 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5103E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.144803E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.9766e-06; norm:  6.3458e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.262413e-06, norm: 3.228337e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.9766e-06; norm:  6.3458e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.288889E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3122, res_abs :  1.4273e-09, res_nor :  9.8567e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2598e-06; norm:  9.3532e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.614157E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2784, res_abs :  1.4270e-09, res_nor :  9.8549e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.2963e-06; norm:  9.3237e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.857660E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2598e-06; norm:  9.3532e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.2963e-06; norm:  9.3237e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.5100E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.270E-01 -0.154E-01  0.500E-02

 Max. velocity at interior face  0.4106E+01 ; min. -0.4309E+01
 Max. velocity at boundary face  0.4512E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415658E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28889E-01    5906   0.59229E-02   0.19950E+00 
c  VelocityX    0.20262E+00     390   0.85709E-01   0.29908E+01 
c  VelocityY    0.20262E+00     390   0.85709E-01   0.30303E+01 
c  VelocityZ    0.20262E+00     390   0.85709E-01   0.67634E-15 
c  Turb Kinetic 0.25714E-02     226   0.13559E-02   0.76614E-03 
c  Turb Dissipa 0.11764E+03     135   0.74012E-04   0.32605E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.080835                             6


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -5099.7          2216.2         -709.58         -370.64
v  Velocity[x]                 -4.4716          4.5468       0.0067306     -0.00072258
v  Velocity[y]                 -4.4188          4.4861        0.043908        0.054014
v  Velocity[z]             -6.7355e-08      1.3409e-07       2.071e-10     -4.2419e-11
v  Turb Kinetic Energy      7.7316e-08         0.21228       0.0037764      0.00076205
v  Turb Dissipation         3.0168e-07          6808.5           12.97           1.344
v  Turb Viscosity           3.8646e-09         0.13866       0.0016689       0.0064919
v  CFL                       0.0003294          142.68           10.46          3.0413
v  Fourier Number            0.0013049          100.91           2.488         0.36982


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022681          153.83          12.948          3.4111


 TIME FOR THE TIME STEP               33:        0.61219E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1735E-07  0.1360E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1408E+03 IN  0.1167E-01  0.2959E-01  0.5000E-02
 COURANT MIN=  0.1066E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

 FOURIER MAX=  0.9414E+02 IN  0.9611E-02 -0.3032E-01  0.5000E-02
 FOURIER MIN=  0.1305E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1520E+03 IN  0.1167E-01  0.2959E-01  0.5000E-02
 COU/FOU MIN=  0.2589E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.0725e-06; norm:  6.3034e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.121361953E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884342E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.171631e-06, norm: 2.459577e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19530E+01 0.10083E+01
   Friction velocity        uet   :  0.30446E-03 0.34782E+00
   Friction velocity        uk    :  0.12678E-02 0.47879E+00
   Dimensionless distance   yplus :  0.18110E-01 0.12060E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1011
   Nb of faces within the viscous sub-layer     :       2431
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         34
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.0728e-06; norm:  6.3025e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.163215e-06, norm: 2.453287e+06, var: Var.  2
 velocity :     263775 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   376, res_abs :  1.9765e-09, res_nor :  9.7671e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.162618e-06, norm: 2.451092e+06, var: Var.  2
 velocity :     251832 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.5031E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.141284E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.0728e-06; norm:  6.3025e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.328247e-06, norm: 3.199782e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.0728e-06; norm:  6.3025e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.286222E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3080, res_abs :  1.4070e-09, res_nor :  9.9590e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1171e-06; norm:  9.5454e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.585752E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2811, res_abs :  1.4105e-09, res_nor :  9.9832e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1338e-06; norm:  9.5152e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.801735E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1171e-06; norm:  9.5454e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1338e-06; norm:  9.5152e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4963E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.269E-01 -0.153E-01  0.500E-02

 Max. velocity at interior face  0.4032E+01 ; min. -0.4379E+01
 Max. velocity at boundary face  0.4711E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415654E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28622E-01    5891   0.56746E-02   0.20259E+00 
c  VelocityX    0.20237E+00     376   0.78274E-01   0.29280E+01 
c  VelocityY    0.20237E+00     376   0.78274E-01   0.29833E+01 
c  VelocityZ    0.20237E+00     376   0.78274E-01   0.71413E-15 
c  Turb Kinetic 0.26117E-02     242   0.15987E-02   0.97565E-03 
c  Turb Dissipa 0.11550E+03     141   0.46380E-04   0.40138E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.057621                             6


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4963.2          2312.3         -722.14         -375.66
v  Velocity[x]                 -4.4238          4.5395         0.00733     -0.00087199
v  Velocity[y]                  -4.362          4.5187         0.04445        0.054022
v  Velocity[z]             -3.4036e-07      2.7818e-07      1.2585e-10     -4.2028e-11
v  Turb Kinetic Energy      8.7393e-08         0.24479       0.0040982      0.00081286
v  Turb Dissipation         3.0944e-07          7695.3          13.872          1.4078
v  Turb Viscosity           1.7347e-08         0.13597       0.0016519       0.0062004
v  CFL                       0.0010663          140.76          10.354          3.0165
v  Fourier Number            0.0013055          94.139           2.639          0.3722


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0025893          152.05          12.993          3.3887


 TIME FOR THE TIME STEP               34:        0.61190E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.4667E-08  0.1977E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1407E+03 IN  0.1176E-01  0.2955E-01  0.5000E-02
 COURANT MIN=  0.1483E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

 FOURIER MAX=  0.8887E+02 IN  0.3058E-01  0.8757E-02  0.5000E-02
 FOURIER MIN=  0.1306E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1561E+03 IN  0.2002E-01 -0.2471E-01  0.5000E-02
 COU/FOU MIN=  0.3005E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.1481e-06; norm:  6.2370e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.209345154E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884346E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.144073e-06, norm: 2.434486e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17875E+01 0.10003E+01
   Friction velocity        uet   :  0.58003E-04 0.33280E+00
   Friction velocity        uk    :  0.12087E-02 0.45955E+00
   Dimensionless distance   yplus :  0.71252E-01 0.12888E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        971
   Nb of faces within the viscous sub-layer     :       2445
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         35
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.1481e-06; norm:  6.2369e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.172122e-06, norm: 2.428062e+06, var: Var.  2
 velocity :     262506 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   369, res_abs :  2.0139e-09, res_nor :  9.9711e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.241948e-06, norm: 2.447555e+06, var: Var.  2
 velocity :     249518 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4902E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.138326E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.1481e-06; norm:  6.2369e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.372755e-06, norm: 3.166475e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.1481e-06; norm:  6.2369e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.282693E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3043, res_abs :  1.3806e-09, res_nor :  9.9807e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1358e-06; norm:  9.7612e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.587540E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2888, res_abs :  1.3762e-09, res_nor :  9.9491e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.1631e-06; norm:  9.7321e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.781717E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1358e-06; norm:  9.7612e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.1631e-06; norm:  9.7321e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4749E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.268E-01 -0.151E-01  0.500E-02

 Max. velocity at interior face  0.4182E+01 ; min. -0.4421E+01
 Max. velocity at boundary face  0.4904E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415651E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28269E-01    5931   0.56513E-02   0.20437E+00 
c  VelocityX    0.20198E+00     369   0.74644E-01   0.28687E+01 
c  VelocityY    0.20198E+00     369   0.74644E-01   0.28942E+01 
c  VelocityZ    0.20198E+00     369   0.74644E-01   0.60250E-15 
c  Turb Kinetic 0.25686E-02     293   0.17858E-02   0.11913E-02 
c  Turb Dissipa 0.11432E+03     151   0.42576E-04   0.52795E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.059055                             9


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4748.5            2380         -722.33         -372.44
v  Velocity[x]                 -4.3701           4.493       0.0073027      -0.0010084
v  Velocity[y]                  -4.293          4.4994        0.044957        0.054021
v  Velocity[z]              -5.771e-07      3.4496e-07      4.2362e-11     -4.0877e-11
v  Turb Kinetic Energy      9.4152e-08         0.24764       0.0044323      0.00086164
v  Turb Dissipation         3.1787e-07           10660          13.932           1.396
v  Turb Viscosity           4.6673e-09         0.19772       0.0016451       0.0059288
v  CFL                       0.0014825          140.67          10.283          2.9924
v  Fourier Number            0.0013061          88.873          2.8179         0.37661


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0030052          156.09          13.101           3.369


 TIME FOR THE TIME STEP               35:        0.61567E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.2413E-08  0.1305E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1429E+03 IN  0.1176E-01  0.2955E-01  0.5000E-02
 COURANT MIN=  0.1731E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.1027E+03 IN -0.2607E-03 -0.1918E-01  0.5000E-02
 FOURIER MIN=  0.1307E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1545E+03 IN  0.2002E-01 -0.2471E-01  0.5000E-02
 COU/FOU MIN=  0.3261E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.1655e-06; norm:  6.1658e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.197324515E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884349E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.212005e-06, norm: 2.425770e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17662E+01 0.98662E+00
   Friction velocity        uet   :  0.86079E-05 0.33639E+00
   Friction velocity        uk    :  0.13850E-02 0.45542E+00
   Dimensionless distance   yplus :  0.37256E-01 0.12955E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        888
   Nb of faces within the viscous sub-layer     :       2393
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         36
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.1659e-06; norm:  6.1648e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.227969e-06, norm: 2.418050e+06, var: Var.  2
 velocity :     259737 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   407, res_abs :  2.0115e-09, res_nor :  9.9766e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.324086e-06, norm: 2.458303e+06, var: Var.  2
 velocity :     247280 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4845E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.135961E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.1659e-06; norm:  6.1648e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.366357e-06, norm: 3.135681e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.1659e-06; norm:  6.1648e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.283178E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3061, res_abs :  1.3522e-09, res_nor :  9.9453e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3610e-06; norm:  9.8735e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.612159E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2889, res_abs :  1.3594e-09, res_nor :  9.9987e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4064e-06; norm:  9.8348e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.803828E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3610e-06; norm:  9.8735e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4064e-06; norm:  9.8348e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4504E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.266E-01 -0.150E-01  0.500E-02

 Max. velocity at interior face  0.4326E+01 ; min. -0.4366E+01
 Max. velocity at boundary face  0.5159E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415651E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@


 Write intermediate restart files
   checkpoint at iteration         36, Physical time    0.36000E-01


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

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

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

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


 Time for restart files:    0.22021E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28318E-01    5950   0.59122E-02   0.20828E+00 
c  VelocityX    0.20162E+00     407   0.76155E-01   0.28373E+01 
c  VelocityY    0.20162E+00     407   0.76155E-01   0.28301E+01 
c  VelocityZ    0.20162E+00     407   0.76155E-01   0.54519E-15 
c  Turb Kinetic 0.24567E-02     352   0.17738E-02   0.14569E-02 
c  Turb Dissipa 0.11421E+03     186   0.10511E-03   0.87585E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.028229                             9


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4504.1            2430         -707.27         -356.81
v  Velocity[x]                  -4.229          4.4211       0.0063118      -0.0011423
v  Velocity[y]                 -4.1553          4.4362        0.045107        0.054027
v  Velocity[z]              -6.216e-07      3.4154e-07     -3.8094e-11     -3.9213e-11
v  Turb Kinetic Energy      1.4431e-07         0.22041       0.0048405       0.0009184
v  Turb Dissipation         3.2656e-07           13883          15.485          1.4874
v  Turb Viscosity            2.413e-09         0.13052       0.0016444       0.0056735
v  CFL                       0.0017311          142.87           10.25          2.9717
v  Fourier Number            0.0013069          102.68          3.0266         0.38258


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0032606          154.46          13.277          3.3543


 TIME FOR THE TIME STEP               36:        0.66483E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1819E-07  0.1276E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1432E+03 IN  0.1176E-01  0.2955E-01  0.5000E-02
 COURANT MIN=  0.1976E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.1223E+03 IN -0.2607E-03 -0.1918E-01  0.5000E-02
 FOURIER MIN=  0.1308E-02 IN  0.3716E-01  0.3114E-01  0.5000E-02

 COU/FOU MAX=  0.1663E+03 IN -0.2471E-01 -0.2002E-01  0.5000E-02
 COU/FOU MIN=  0.3506E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.1276e-06; norm:  6.0916e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.282767801E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884349E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.272882e-06, norm: 2.439857e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19208E+01 0.98796E+00
   Friction velocity        uet   :  0.32571E-04 0.34734E+00
   Friction velocity        uk    :  0.91989E-03 0.44779E+00
   Dimensionless distance   yplus :  0.32053E-01 0.12167E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        856
   Nb of faces within the viscous sub-layer     :       2347
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         37
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.1277e-06; norm:  6.0914e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.249269e-06, norm: 2.425341e+06, var: Var.  2
 velocity :     257828 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   444, res_abs :  1.9664e-09, res_nor :  9.7644e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.216083e-06, norm: 2.479778e+06, var: Var.  2
 velocity :     247063 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4801E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.134434E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.1277e-06; norm:  6.0914e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.279563e-06, norm: 3.100062e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.1277e-06; norm:  6.0914e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.272583E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3058, res_abs :  1.3356e-09, res_nor :  9.9349e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.5983e-06; norm:  9.7762e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.634226E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2776, res_abs :  1.3340e-09, res_nor :  9.9234e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6502e-06; norm:  9.7168e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.853155E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5983e-06; norm:  9.7762e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6502e-06; norm:  9.7168e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4524E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.263E-01 -0.147E-01  0.500E-02

 Max. velocity at interior face  0.4357E+01 ; min. -0.4367E+01
 Max. velocity at boundary face  0.5412E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415635E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27258E-01    5834   0.63463E-02   0.20276E+00 
c  VelocityX    0.20138E+00     444   0.67440E-01   0.28327E+01 
c  VelocityY    0.20138E+00     444   0.67440E-01   0.28178E+01 
c  VelocityZ    0.20138E+00     444   0.67440E-01   0.53910E-15 
c  Turb Kinetic 0.23813E-02     351   0.20406E-02   0.17670E-02 
c  Turb Dissipa 0.11817E+03     198   0.26380E-03   0.20979E+07 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.027806                             7


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4524.2          2433.2         -689.23         -340.74
v  Velocity[x]                 -4.0714          4.3287       0.0042867      -0.0012729
v  Velocity[y]                 -4.0257          4.3541        0.043974        0.054035
v  Velocity[z]              -5.259e-07      2.9206e-07      -1.118e-10     -3.7388e-11
v  Turb Kinetic Energy      1.9153e-07         0.18004       0.0052447      0.00097619
v  Turb Dissipation         3.3593e-07           15119          19.185          1.6802
v  Turb Viscosity           1.8194e-08         0.12762        0.001643       0.0054337
v  CFL                       0.0019761           143.2          10.249          2.9581
v  Fourier Number            0.0013078          122.34          3.2043         0.38757


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0035057          166.26          13.454          3.3457


 TIME FOR THE TIME STEP               37:        0.63685E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1943E-07  0.1246E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1403E+03 IN  0.1185E-01  0.2952E-01  0.5000E-02
 COURANT MIN=  0.2229E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.1310E+03 IN -0.2607E-03 -0.1918E-01  0.5000E-02
 FOURIER MIN=  0.1309E-02 IN -0.1846E-02  0.4850E-01  0.5000E-02

 COU/FOU MAX=  0.1649E+03 IN  0.4094E-04 -0.1918E-01  0.5000E-02
 COU/FOU MIN=  0.3758E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.0772e-06; norm:  6.0180e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813         0.471455043E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884365E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.173721e-06, norm: 2.466286e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20014E+01 0.10564E+01
   Friction velocity        uet   :  0.29962E-04 0.35433E+00
   Friction velocity        uk    :  0.15201E-02 0.46407E+00
   Dimensionless distance   yplus :  0.36231E-01 0.11935E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        837
   Nb of faces within the viscous sub-layer     :       2315
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         38
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.0773e-06; norm:  6.0177e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.127755e-06, norm: 2.470756e+06, var: Var.  2
 velocity :     257371 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   444, res_abs :  1.9679e-09, res_nor :  9.7770e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.117165e-06, norm: 2.546746e+06, var: Var.  2
 velocity :     246844 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4773E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.133669E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.0773e-06; norm:  6.0177e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.153767e-06, norm: 3.138045e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.0773e-06; norm:  6.0177e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.264715E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3077, res_abs :  1.3232e-09, res_nor :  9.8992e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6777e-06; norm:  9.7833e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.641312E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2898, res_abs :  1.3191e-09, res_nor :  9.8682e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7486e-06; norm:  9.7075e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.883025E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6777e-06; norm:  9.7833e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7486e-06; norm:  9.7075e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4546E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.258E-01 -0.177E-01  0.500E-02

 Max. velocity at interior face  0.4078E+01 ; min. -0.4342E+01
 Max. velocity at boundary face  0.5692E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415641E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26472E-01    5975   0.66060E-02   0.19804E+00 
c  VelocityX    0.20128E+00     444   0.65167E-01   0.28535E+01 
c  VelocityY    0.20128E+00     444   0.65167E-01   0.28510E+01 
c  VelocityZ    0.20128E+00     444   0.65167E-01   0.51940E-15 
c  Turb Kinetic 0.24371E-02     357   0.20919E-02   0.19164E-02 
c  Turb Dissipa 0.12992E+03     277   0.51343E-03   0.34259E+07 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.032971                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4546.2          2410.3         -659.72          -315.8
v  Velocity[x]                 -4.0417          4.1379       0.0015177      -0.0014094
v  Velocity[y]                 -4.0164          4.1858        0.041563        0.054033
v  Velocity[z]             -3.5125e-07      2.5555e-07     -1.7343e-10      -3.603e-11
v  Turb Kinetic Energy      2.5991e-07         0.19765       0.0054242       0.0010276
v  Turb Dissipation         3.4456e-07           20468          23.788          1.9964
v  Turb Viscosity           1.9429e-08         0.12465       0.0016304       0.0052082
v  CFL                       0.0022285          140.28          10.283          2.9519
v  Fourier Number            0.0013089          130.99          3.2858         0.38843


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0037584          164.93          13.569          3.3404


 TIME FOR THE TIME STEP               38:        0.65004E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1497E-07  0.1217E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1342E+03 IN  0.1185E-01  0.2952E-01  0.5000E-02
 COURANT MIN=  0.2457E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.1067E+03 IN -0.2252E-01 -0.2246E-01  0.5000E-02
 FOURIER MIN=  0.1308E-02 IN -0.1846E-02  0.4850E-01  0.5000E-02

 COU/FOU MAX=  0.1511E+03 IN -0.2490E-01 -0.1979E-01  0.5000E-02
 COU/FOU MIN=  0.3987E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.0204e-06; norm:  5.9422e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.181151804E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884359E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.067298e-06, norm: 2.542023e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20134E+01 0.10636E+01
   Friction velocity        uet   :  0.17484E-03 0.35388E+00
   Friction velocity        uk    :  0.11032E-02 0.47049E+00
   Dimensionless distance   yplus :  0.61161E-01 0.11886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        827
   Nb of faces within the viscous sub-layer     :       2215
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         39
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.0205e-06; norm:  5.9421e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.196798e-06, norm: 2.531448e+06, var: Var.  2
 velocity :     256656 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   411, res_abs :  2.0060e-09, res_nor :  9.9598e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.252558e-06, norm: 2.610164e+06, var: Var.  2
 velocity :     246522 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4779E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.133271E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  2.0205e-06; norm:  5.9421e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.218070e-06, norm: 3.167003e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.0205e-06; norm:  5.9421e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.273533E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3160, res_abs :  1.3224e-09, res_nor :  9.9226e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7806e-06; norm:  1.0082e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.654224E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2899, res_abs :  1.3325e-09, res_nor :  9.9988e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.8745e-06; norm:  9.9840e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.920367E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7806e-06; norm:  1.0082e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8745e-06; norm:  9.9840e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4559E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.259E-01 -0.176E-01  0.500E-02

 Max. velocity at interior face  0.4054E+01 ; min. -0.4247E+01
 Max. velocity at boundary face  0.5964E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415640E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27353E-01    6059   0.69060E-02   0.20525E+00 
c  VelocityX    0.20142E+00     411   0.64634E-01   0.29552E+01 
c  VelocityY    0.20142E+00     411   0.64634E-01   0.29301E+01 
c  VelocityZ    0.20142E+00     411   0.64634E-01   0.54644E-15 
c  Turb Kinetic 0.25524E-02     284   0.21468E-02   0.25756E-02 
c  Turb Dissipa 0.13981E+03     176   0.52183E-03   0.35112E+07 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.033254                             5


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4559.3          2364.2         -636.58         -297.09
v  Velocity[x]                 -4.0099          4.0922      -0.0014597      -0.0015496
v  Velocity[y]                 -3.9836          3.9587        0.038333        0.054019
v  Velocity[z]             -1.4675e-07      2.1299e-07     -2.2038e-10     -3.5841e-11
v  Turb Kinetic Energy      3.3791e-07         0.17525       0.0050477       0.0010285
v  Turb Dissipation         3.5373e-07           12686          23.265          1.9589
v  Turb Viscosity           1.4972e-08         0.12169       0.0015495       0.0049899
v  CFL                       0.0024571          134.16          10.379          2.9555
v  Fourier Number            0.0013078          106.72          2.9653         0.36954


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0039873          151.05          13.344           3.325


 TIME FOR THE TIME STEP               39:        0.63228E+01

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


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



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3404E-07  0.1186E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1215E+03 IN  0.1185E-01  0.2952E-01  0.5000E-02
 COURANT MIN=  0.2552E-02 IN  0.3240E-01 -0.3618E-01  0.5000E-02

 FOURIER MAX=  0.1082E+03 IN -0.2252E-01 -0.2246E-01  0.5000E-02
 FOURIER MIN=  0.1307E-02 IN -0.1846E-02  0.4850E-01  0.5000E-02

 COU/FOU MAX=  0.1450E+03 IN -0.2490E-01 -0.1979E-01  0.5000E-02
 COU/FOU MIN=  0.4174E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.9374e-06; norm:  5.8585e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.199591891E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884360E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.193542e-06, norm: 2.609656e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19641E+01 0.99272E+00
   Friction velocity        uet   :  0.36265E-04 0.36759E+00
   Friction velocity        uk    :  0.11346E-02 0.47432E+00
   Dimensionless distance   yplus :  0.51521E-01 0.11830E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        796
   Nb of faces within the viscous sub-layer     :       2127
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         40
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.9374e-06; norm:  5.8584e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.149164e-06, norm: 2.619579e+06, var: Var.  2
 velocity :     256013 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   407, res_abs :  1.9542e-09, res_nor :  9.6904e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.193563e-06, norm: 2.700195e+06, var: Var.  2
 velocity :     246298 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4670E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.133370E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.9374e-06; norm:  5.8584e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.196216e-06, norm: 3.229998e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.9374e-06; norm:  5.8584e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.282016E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3176, res_abs :  1.3246e-09, res_nor :  9.9318e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.8046e-06; norm:  1.0433e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.659885E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2893, res_abs :  1.3307e-09, res_nor :  9.9774e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.9172e-06; norm:  1.0313e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.948612E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8046e-06; norm:  1.0433e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.9172e-06; norm:  1.0313e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4575E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.259E-01 -0.174E-01  0.500E-02

 Max. velocity at interior face  0.4313E+01 ; min. -0.3982E+01
 Max. velocity at boundary face  0.6255E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415643E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28202E-01    6069   0.71126E-02   0.21145E+00 
c  VelocityX    0.20166E+00     407   0.63976E-01   0.30556E+01 
c  VelocityY    0.20166E+00     407   0.63976E-01   0.29891E+01 
c  VelocityZ    0.20166E+00     407   0.63976E-01   0.50512E-15 
c  Turb Kinetic 0.26957E-02     270   0.16275E-02   0.23144E-02 
c  Turb Dissipa 0.15075E+03     167   0.26269E-03   0.21325E+07 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.034703                             5


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4574.8          2298.3         -614.42         -281.54
v  Velocity[x]                 -3.9723          4.0625      -0.0045552      -0.0016662
v  Velocity[y]                 -3.9376          3.8421         0.03607        0.054001
v  Velocity[z]              -5.777e-08      2.3903e-07        -2.5e-10      -3.722e-11
v  Turb Kinetic Energy      3.3428e-07         0.18138       0.0046647       0.0010309
v  Turb Dissipation          3.627e-07           10953          21.599           1.914
v  Turb Viscosity           3.4041e-08         0.11859       0.0015027       0.0047869
v  CFL                       0.0025521          121.52          10.515          2.9676
v  Fourier Number            0.0013074          108.22          2.8554         0.36098


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.004174          145.04           13.37          3.3286


 TIME FOR THE TIME STEP               40:        0.63179E+01

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


 INSTANT    0.410000000E-01   TIME STEP NUMBER              41
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3273E-07  0.3222E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1165E+03 IN -0.6933E-02 -0.3104E-01  0.5000E-02
 COURANT MIN=  0.2646E-02 IN -0.1172E-01 -0.4722E-01  0.5000E-02

 FOURIER MAX=  0.8586E+02 IN -0.2362E-01 -0.2130E-01  0.5000E-02
 FOURIER MIN=  0.1308E-02 IN -0.1846E-02  0.4850E-01  0.5000E-02

 COU/FOU MAX=  0.1422E+03 IN -0.2490E-01 -0.1979E-01  0.5000E-02
 COU/FOU MIN=  0.4290E-02 IN -0.1172E-01 -0.4722E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8317e-06; norm:  5.7784e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.284776007E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884357E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.196024e-06, norm: 2.701676e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21759E+01 0.97993E+00
   Friction velocity        uet   :  0.30318E-03 0.38506E+00
   Friction velocity        uk    :  0.96866E-03 0.47988E+00
   Dimensionless distance   yplus :  0.88078E-01 0.11783E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        794
   Nb of faces within the viscous sub-layer     :       2095
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         41
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.8317e-06; norm:  5.7786e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.146509e-06, norm: 2.717014e+06, var: Var.  2
 velocity :     255249 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   391, res_abs :  1.9755e-09, res_nor :  9.7027e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.175300e-06, norm: 2.782626e+06, var: Var.  2
 velocity :     247156 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4563E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.133892E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.8317e-06; norm:  5.7786e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.185968e-06, norm: 3.288765e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8317e-06; norm:  5.7786e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.286213E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3185, res_abs :  1.3336e-09, res_nor :  9.9603e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6416e-06; norm:  1.0727e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.643572E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2830, res_abs :  1.3296e-09, res_nor :  9.9305e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7485e-06; norm:  1.0625e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.932699E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6416e-06; norm:  1.0727e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7485e-06; norm:  1.0625e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4597E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.257E-01 -0.172E-01  0.500E-02

 Max. velocity at interior face  0.4519E+01 ; min. -0.3995E+01
 Max. velocity at boundary face  0.6540E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415656E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28621E-01    6015   0.69661E-02   0.21376E+00 
c  VelocityX    0.20361E+00     391   0.63776E-01   0.31143E+01 
c  VelocityY    0.20361E+00     391   0.63776E-01   0.30414E+01 
c  VelocityZ    0.20361E+00     391   0.63776E-01   0.47003E-15 
c  Turb Kinetic 0.28096E-02     255   0.13495E-02   0.21146E-02 
c  Turb Dissipa 0.15884E+03     181   0.11808E-03   0.90773E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation            -4.0581                             9


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4596.7          2430.9         -603.68         -275.25
v  Velocity[x]                 -3.9309          4.1925       -0.007429      -0.0017872
v  Velocity[y]                 -3.9506          3.8363        0.035169        0.053981
v  Velocity[z]              -5.354e-08      2.6998e-07     -2.6404e-10     -4.0083e-11
v  Turb Kinetic Energy      3.4128e-07         0.20493       0.0043348       0.0010295
v  Turb Dissipation         3.7196e-07          9429.7          19.792          1.7968
v  Turb Viscosity           3.2726e-08         0.32219        0.001461       0.0045972
v  CFL                       0.0026459          116.49          10.651          2.9831
v  Fourier Number            0.0013081          85.864          2.7461         0.35286


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0042899          142.18          13.397           3.336


 TIME FOR THE TIME STEP               41:        0.64162E+01

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


 INSTANT    0.420000000E-01   TIME STEP NUMBER              42
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1721E-07  0.1126E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1193E+03 IN  0.7319E-02 -0.3095E-01  0.5000E-02
 COURANT MIN=  0.2820E-02 IN -0.1172E-01 -0.4722E-01  0.5000E-02

 FOURIER MAX=  0.8822E+02 IN -0.2821E-02 -0.3168E-01  0.5000E-02
 FOURIER MIN=  0.1310E-02 IN -0.1846E-02  0.4850E-01  0.5000E-02

 COU/FOU MAX=  0.1354E+03 IN  0.7319E-02 -0.3095E-01  0.5000E-02
 COU/FOU MIN=  0.4410E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7622e-06; norm:  5.7098e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.415181770E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884344E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.192486e-06, norm: 2.788210e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22250E+01 0.93603E+00
   Friction velocity        uet   :  0.28017E-03 0.39037E+00
   Friction velocity        uk    :  0.13488E-02 0.49318E+00
   Dimensionless distance   yplus :  0.67790E-01 0.11722E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        745
   Nb of faces within the viscous sub-layer     :       2106
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         42
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.7622e-06; norm:  5.7099e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.136076e-06, norm: 2.790228e+06, var: Var.  2
 velocity :     255951 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   388, res_abs :  2.0090e-09, res_nor :  9.9068e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.096408e-06, norm: 2.840541e+06, var: Var.  2
 velocity :     247727 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4453E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.135539E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.7622e-06; norm:  5.7099e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.135454e-06, norm: 3.333918e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7622e-06; norm:  5.7099e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.277295E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3111, res_abs :  1.3537e-09, res_nor :  9.9872e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.9255e-06; norm:  1.0702e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.636019E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2870, res_abs :  1.3543e-09, res_nor :  9.9916e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  2.0416e-06; norm:  1.0650e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.915517E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.9255e-06; norm:  1.0702e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  2.0416e-06; norm:  1.0650e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4610E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.256E-01 -0.173E-01  0.500E-02

 Max. velocity at interior face  0.4791E+01 ; min. -0.4112E+01
 Max. velocity at boundary face  0.6800E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415657E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27729E-01    5981   0.67546E-02   0.20459E+00 
c  VelocityX    0.20279E+00     388   0.62870E-01   0.32018E+01 
c  VelocityY    0.20279E+00     388   0.62870E-01   0.31173E+01 
c  VelocityZ    0.20279E+00     388   0.62870E-01   0.44593E-15 
c  Turb Kinetic 0.29043E-02     266   0.12690E-02   0.13022E-02 
c  Turb Dissipa 0.16707E+03     165   0.19025E-03   0.11387E+07 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.031482                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                      -4610          2531.7         -597.51         -274.28
v  Velocity[x]                 -3.8861          4.3408       -0.010142      -0.0019073
v  Velocity[y]                 -3.9775          3.8352         0.03447        0.053966
v  Velocity[z]             -6.1703e-08      3.1404e-07     -2.6731e-10     -4.4116e-11
v  Turb Kinetic Energy      3.9658e-07         0.21364        0.004172       0.0010408
v  Turb Dissipation          3.816e-07           15204          21.792          1.9053
v  Turb Viscosity           1.7209e-08         0.11264       0.0014166       0.0044136
v  CFL                       0.0028195          119.26          10.735           2.995
v  Fourier Number              0.00131          88.222          2.6058         0.34356


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0044104          135.37          13.341          3.3385


 TIME FOR THE TIME STEP               42:        0.62444E+01

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


 INSTANT    0.430000000E-01   TIME STEP NUMBER              43
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.6030E-08  0.1098E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1321E+03 IN  0.7319E-02 -0.3095E-01  0.5000E-02
 COURANT MIN=  0.2905E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.7091E+02 IN -0.3118E-02 -0.3165E-01  0.5000E-02
 FOURIER MIN=  0.1312E-02 IN -0.3636E-02  0.4841E-01  0.5000E-02

 COU/FOU MAX=  0.1462E+03 IN  0.7319E-02 -0.3095E-01  0.5000E-02
 COU/FOU MIN=  0.4438E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6444e-06; norm:  5.6704e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.193600093E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884343E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.110211e-06, norm: 2.842963e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24053E+01 0.97496E+00
   Friction velocity        uet   :  0.18857E-03 0.40412E+00
   Friction velocity        uk    :  0.13088E-02 0.50070E+00
   Dimensionless distance   yplus :  0.21003E-01 0.12180E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        690
   Nb of faces within the viscous sub-layer     :       2105
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         43
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.6444e-06; norm:  5.6706e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.152057e-06, norm: 2.851081e+06, var: Var.  2
 velocity :     256754 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   394, res_abs :  2.0299e-09, res_nor :  9.9755e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.145644e-06, norm: 2.881645e+06, var: Var.  2
 velocity :     248352 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4324E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.137596E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.6444e-06; norm:  5.6706e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.182713e-06, norm: 3.361305e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6444e-06; norm:  5.6706e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.270042E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3088, res_abs :  1.3679e-09, res_nor :  9.9414e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.8148e-06; norm:  1.0549e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.651179E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2855, res_abs :  1.3714e-09, res_nor :  9.9672e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.8931e-06; norm:  1.0515e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.934279E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8148e-06; norm:  1.0549e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8931e-06; norm:  1.0515e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4612E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.254E-01 -0.170E-01  0.500E-02

 Max. velocity at interior face  0.4875E+01 ; min. -0.4162E+01
 Max. velocity at boundary face  0.7037E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415657E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27004E-01    5943   0.67900E-02   0.19626E+00 
c  VelocityX    0.20349E+00     394   0.63366E-01   0.32750E+01 
c  VelocityY    0.20349E+00     394   0.63366E-01   0.31627E+01 
c  VelocityZ    0.20349E+00     394   0.63366E-01   0.43349E-15 
c  Turb Kinetic 0.29438E-02     282   0.12236E-02   0.12863E-02 
c  Turb Dissipa 0.17556E+03     164   0.79671E-04   0.95379E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.029047                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                      -4612          2595.2          -594.2         -274.17
v  Velocity[x]                 -3.9121          4.3059       -0.012627      -0.0019993
v  Velocity[y]                 -4.0048          3.7876         0.03383        0.053966
v  Velocity[z]             -7.0853e-08      3.4603e-07     -2.6726e-10     -4.8901e-11
v  Turb Kinetic Energy      4.0815e-07          0.2099       0.0040233       0.0010529
v  Turb Dissipation         3.9189e-07          8518.8          20.313          1.8196
v  Turb Viscosity           6.0305e-09         0.10977       0.0013857        0.004241
v  CFL                       0.0029053          132.05          10.783           3.002
v  Fourier Number            0.0013125          70.912           2.508         0.33703


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0044377          146.24          13.291           3.339


 TIME FOR THE TIME STEP               43:        0.62162E+01

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


 INSTANT    0.440000000E-01   TIME STEP NUMBER              44
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.4681E-08  0.1071E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1347E+03 IN  0.7319E-02 -0.3095E-01  0.5000E-02
 COURANT MIN=  0.2870E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.9073E+02 IN -0.6157E-02 -0.3120E-01  0.5000E-02
 FOURIER MIN=  0.1312E-02 IN -0.3636E-02  0.4841E-01  0.5000E-02

 COU/FOU MAX=  0.1604E+03 IN -0.7126E-02 -0.3100E-01  0.5000E-02
 COU/FOU MIN=  0.4403E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5609e-06; norm:  5.6551e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.519552644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884343E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 2.135295e-06, norm: 2.882105e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25496E+01 0.10070E+01
   Friction velocity        uet   :  0.17539E-03 0.40570E+00
   Friction velocity        uk    :  0.13173E-02 0.49619E+00
   Dimensionless distance   yplus :  0.38795E-01 0.12562E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        641
   Nb of faces within the viscous sub-layer     :       2116
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         44
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.5608e-06; norm:  5.6554e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 2.023510e-06, norm: 2.889157e+06, var: Var.  2
 velocity :     256877 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   405, res_abs :  2.0221e-09, res_nor :  9.9015e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.950716e-06, norm: 2.905784e+06, var: Var.  2
 velocity :     249233 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4416E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.139383E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.5608e-06; norm:  5.6554e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.119957e-06, norm: 3.371052e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5608e-06; norm:  5.6554e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.262698E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3124, res_abs :  1.3855e-09, res_nor :  9.9400e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6108e-06; norm:  1.0286e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.667973E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2829, res_abs :  1.3803e-09, res_nor :  9.9030e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6906e-06; norm:  1.0228e-02
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.970023E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6108e-06; norm:  1.0286e-02
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6906e-06; norm:  1.0228e-02

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4604E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.244E-01 -0.194E-01  0.500E-02

 Max. velocity at interior face  0.4698E+01 ; min. -0.4061E+01
 Max. velocity at boundary face  0.7235E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415658E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26270E-01    5953   0.69594E-02   0.18847E+00 
c  VelocityX    0.20422E+00     405   0.62662E-01   0.33504E+01 
c  VelocityY    0.20422E+00     405   0.62662E-01   0.32366E+01 
c  VelocityZ    0.20422E+00     405   0.62662E-01   0.40956E-15 
c  Turb Kinetic 0.29085E-02     298   0.14275E-02   0.93047E-03 
c  Turb Dissipa 0.17860E+03     198   0.15970E-03   0.86784E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.036143                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4603.7          2639.6         -589.76          -271.6
v  Velocity[x]                  -4.007           4.079       -0.014238       -0.002077
v  Velocity[y]                 -4.0381          3.7989        0.033072        0.053968
v  Velocity[z]             -6.6434e-08      3.4278e-07     -2.7252e-10     -5.4118e-11
v  Turb Kinetic Energy      4.6097e-07         0.18775       0.0040222       0.0010752
v  Turb Dissipation         4.0314e-07           13620          21.116          1.8934
v  Turb Viscosity           4.6813e-09         0.10712       0.0013693       0.0040774
v  CFL                       0.0028695           134.7          10.802          3.0023
v  Fourier Number            0.0013115          90.725          2.4549         0.33329


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0044027          160.39          13.257          3.3356


 TIME FOR THE TIME STEP               44:        0.62655E+01

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


 INSTANT    0.450000000E-01   TIME STEP NUMBER              45
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1986E-07  0.1046E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1302E+03 IN  0.7319E-02 -0.3095E-01  0.5000E-02
 COURANT MIN=  0.2776E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.8073E+02 IN -0.6059E-02 -0.3122E-01  0.5000E-02
 FOURIER MIN=  0.1310E-02 IN  0.1645E-01  0.4560E-01  0.5000E-02

 COU/FOU MAX=  0.1620E+03 IN -0.7319E-02 -0.3095E-01  0.5000E-02
 COU/FOU MIN=  0.4310E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5067e-06; norm:  5.6531e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.468760189E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884342E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 1.971956e-06, norm: 2.905073e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27496E+01 0.10148E+01
   Friction velocity        uet   :  0.30496E-03 0.38511E+00
   Friction velocity        uk    :  0.14217E-02 0.48896E+00
   Dimensionless distance   yplus :  0.51894E-01 0.12795E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        624
   Nb of faces within the viscous sub-layer     :       2128
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         45
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.5066e-06; norm:  5.6534e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.981303e-06, norm: 2.906832e+06, var: Var.  2
 velocity :     257791 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   395, res_abs :  2.0301e-09, res_nor :  9.9030e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.884544e-06, norm: 2.911382e+06, var: Var.  2
 velocity :     249881 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4415E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.140702E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.5066e-06; norm:  5.6534e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.121512e-06, norm: 3.366507e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5066e-06; norm:  5.6534e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.257609E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3176, res_abs :  1.3990e-09, res_nor :  9.9427e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6897e-06; norm:  9.8783e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.667308E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2824, res_abs :  1.4048e-09, res_nor :  9.9841e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7957e-06; norm:  9.8197e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.994911E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6897e-06; norm:  9.8783e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7957e-06; norm:  9.8197e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4591E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.697E-02 -0.306E-01  0.500E-02

 Max. velocity at interior face  0.4413E+01 ; min. -0.4070E+01
 Max. velocity at boundary face  0.7402E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415646E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25761E-01    6000   0.70710E-02   0.18309E+00 
c  VelocityX    0.20500E+00     395   0.61645E-01   0.34145E+01 
c  VelocityY    0.20500E+00     395   0.61645E-01   0.33110E+01 
c  VelocityZ    0.20500E+00     395   0.61645E-01   0.38729E-15 
c  Turb Kinetic 0.28778E-02     315   0.14839E-02   0.10309E-02 
c  Turb Dissipa 0.18029E+03     209   0.12184E-03   0.10635E+07 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.032676                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4591.1          2665.8         -579.94         -262.32
v  Velocity[x]                  -4.064          3.9522       -0.014819      -0.0021259
v  Velocity[y]                 -4.0677          3.8387        0.031901        0.053983
v  Velocity[z]             -8.4521e-08      3.3967e-07     -2.8881e-10     -5.9783e-11
v  Turb Kinetic Energy      5.3416e-07         0.21534       0.0040475       0.0010947
v  Turb Dissipation          4.156e-07           14513          20.839          1.8376
v  Turb Viscosity           1.9863e-08         0.10456       0.0013609       0.0039214
v  CFL                       0.0027764           130.2          10.773          2.9941
v  Fourier Number            0.0013104          80.726          2.4254         0.33113


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0043104          162.01          13.198          3.3253


 TIME FOR THE TIME STEP               45:        0.62560E+01

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


 INSTANT    0.460000000E-01   TIME STEP NUMBER              46
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.3341E-07  0.1021E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1244E+03 IN  0.7222E-02 -0.3098E-01  0.5000E-02
 COURANT MIN=  0.2616E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.6597E+02 IN -0.7608E-02 -0.3088E-01  0.5000E-02
 FOURIER MIN=  0.1309E-02 IN  0.1645E-01  0.4560E-01  0.5000E-02

 COU/FOU MAX=  0.1359E+03 IN  0.7222E-02 -0.3098E-01  0.5000E-02
 COU/FOU MIN=  0.4151E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4484e-06; norm:  5.6584e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813         0.120756559E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884354E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 1.934693e-06, norm: 2.906661e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28320E+01 0.99919E+00
   Friction velocity        uet   :  0.46301E-03 0.36234E+00
   Friction velocity        uk    :  0.13909E-02 0.48990E+00
   Dimensionless distance   yplus :  0.22716E-01 0.12850E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        621
   Nb of faces within the viscous sub-layer     :       2177
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         46
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4484e-06; norm:  5.6584e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.932818e-06, norm: 2.911619e+06, var: Var.  2
 velocity :     258205 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   387, res_abs :  2.0045e-09, res_nor :  9.7420e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.831717e-06, norm: 2.902072e+06, var: Var.  2
 velocity :     251544 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4396E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.141962E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4484e-06; norm:  5.6584e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.099926e-06, norm: 3.361463e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4484e-06; norm:  5.6584e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.244807E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3169, res_abs :  1.4166e-09, res_nor :  9.9786e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6980e-06; norm:  9.3585e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.647107E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2807, res_abs :  1.4187e-09, res_nor :  9.9934e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7887e-06; norm:  9.3203e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.968063E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6980e-06; norm:  9.3585e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7887e-06; norm:  9.3203e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4569E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.685E-02 -0.305E-01  0.500E-02

 Max. velocity at interior face  0.4077E+01 ; min. -0.4067E+01
 Max. velocity at boundary face  0.7531E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415634E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24481E-01    5976   0.68192E-02   0.17245E+00 
c  VelocityX    0.20576E+00     387   0.61836E-01   0.34594E+01 
c  VelocityY    0.20576E+00     387   0.61836E-01   0.33421E+01 
c  VelocityZ    0.20576E+00     387   0.61836E-01   0.33099E-15 
c  Turb Kinetic 0.28566E-02     317   0.13019E-02   0.93546E-03 
c  Turb Dissipa 0.17993E+03     197   0.50425E-04   0.46951E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.034841                             6


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4569.1          2684.2         -567.34         -248.19
v  Velocity[x]                 -4.0989          3.9893       -0.014998      -0.0021277
v  Velocity[y]                 -4.0994          3.8871        0.030073        0.053995
v  Velocity[z]             -1.0214e-07      3.4875e-07     -3.1519e-10     -6.5449e-11
v  Turb Kinetic Energy      6.5308e-07         0.23228        0.004062       0.0011164
v  Turb Dissipation         4.2922e-07          5139.6          19.214          1.7517
v  Turb Viscosity           3.3415e-08         0.10209       0.0013596       0.0037739
v  CFL                       0.0026158          124.43          10.717          2.9806
v  Fourier Number            0.0013089          65.974          2.4118         0.33029


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0041508          135.89          13.129          3.3109


 TIME FOR THE TIME STEP               46:        0.63009E+01

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


 INSTANT    0.470000000E-01   TIME STEP NUMBER              47
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.5548E-07  0.9967E-01
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1178E+03 IN  0.7222E-02 -0.3098E-01  0.5000E-02
 COURANT MIN=  0.2908E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

 FOURIER MAX=  0.5700E+02 IN -0.1203E-01 -0.2944E-01  0.5000E-02
 FOURIER MIN=  0.1308E-02 IN  0.1645E-01  0.4560E-01  0.5000E-02

 COU/FOU MAX=  0.1292E+03 IN  0.7222E-02 -0.3098E-01  0.5000E-02
 COU/FOU MIN=  0.4444E-02 IN -0.9767E-02 -0.4757E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4126e-06; norm:  5.6633e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813         0.285119548E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884366E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 1.867280e-06, norm: 2.893556e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27442E+01 0.96658E+00
   Friction velocity        uet   :  0.62879E-03 0.35176E+00
   Friction velocity        uk    :  0.77344E-03 0.48673E+00
   Dimensionless distance   yplus :  0.28880E-01 0.12811E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        617
   Nb of faces within the viscous sub-layer     :       2192
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         47
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4126e-06; norm:  5.6633e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.875727e-06, norm: 2.888269e+06, var: Var.  2
 velocity :     260104 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   388, res_abs :  1.9934e-09, res_nor :  9.6511e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.826750e-06, norm: 2.875504e+06, var: Var.  2
 velocity :     251478 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4415E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.142764E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4126e-06; norm:  5.6633e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.136179e-06, norm: 3.336941e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4126e-06; norm:  5.6633e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.235222E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3133, res_abs :  1.4275e-09, res_nor :  9.9989e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.7505e-06; norm:  9.0050e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.613314E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2883, res_abs :  1.4177e-09, res_nor :  9.9307e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.8370e-06; norm:  8.9833e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.905323E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.7505e-06; norm:  9.0050e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.8370e-06; norm:  8.9833e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4555E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.695E-02 -0.305E-01  0.500E-02

 Max. velocity at interior face  0.3803E+01 ; min. -0.3974E+01
 Max. velocity at boundary face  0.7619E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415650E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23522E-01    6016   0.63414E-02   0.16476E+00 
c  VelocityX    0.20654E+00     388   0.58978E-01   0.34038E+01 
c  VelocityY    0.20654E+00     388   0.58978E-01   0.33243E+01 
c  VelocityZ    0.20654E+00     388   0.58978E-01   0.33882E-15 
c  Turb Kinetic 0.28257E-02     308   0.10352E-02   0.66045E-03 
c  Turb Dissipa 0.17673E+03     190   0.28163E-04   0.83294E+05 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.046472                             7


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4555.3          2672.2         -556.61         -233.61
v  Velocity[x]                 -4.0989          4.0247       -0.014976      -0.0021062
v  Velocity[y]                 -4.1217          3.9348        0.027513        0.054007
v  Velocity[z]             -1.1911e-07      3.5729e-07     -3.4509e-10     -7.0625e-11
v  Turb Kinetic Energy      8.1339e-07         0.21966       0.0041555       0.0011418
v  Turb Dissipation         4.4281e-07          5183.3           19.03          1.7432
v  Turb Viscosity            5.548e-08        0.099673       0.0013669       0.0036344
v  CFL                       0.0029084          117.84          10.653          2.9667
v  Fourier Number            0.0013076          57.003          2.4324         0.33132


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0044444          129.16          13.085           3.298


 TIME FOR THE TIME STEP               47:        0.62448E+01

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


 INSTANT    0.480000000E-01   TIME STEP NUMBER              48
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1082E-07  0.9730E-01
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1124E+03 IN  0.7126E-02 -0.3100E-01  0.5000E-02
 COURANT MIN=  0.3327E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

 FOURIER MAX=  0.6397E+02 IN -0.1203E-01 -0.2944E-01  0.5000E-02
 FOURIER MIN=  0.1306E-02 IN  0.1645E-01  0.4560E-01  0.5000E-02

 COU/FOU MAX=  0.1233E+03 IN  0.7126E-02 -0.3100E-01  0.5000E-02
 COU/FOU MIN=  0.4859E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4045e-06; norm:  5.6544e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.119770429E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884350E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 1.834476e-06, norm: 2.863658e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26665E+01 0.99236E+00
   Friction velocity        uet   :  0.69638E-04 0.33807E+00
   Friction velocity        uk    :  0.97626E-03 0.48538E+00
   Dimensionless distance   yplus :  0.12050E-01 0.12684E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        600
   Nb of faces within the viscous sub-layer     :       2178
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         48
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4045e-06; norm:  5.6544e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.847353e-06, norm: 2.856924e+06, var: Var.  2
 velocity :     260660 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   388, res_abs :  2.0338e-09, res_nor :  9.8096e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.880253e-06, norm: 2.844721e+06, var: Var.  2
 velocity :     250205 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4421E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.143223E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4045e-06; norm:  5.6544e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.193344e-06, norm: 3.319158e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4045e-06; norm:  5.6544e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.228744E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3095, res_abs :  1.4285e-09, res_nor :  9.9741e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6091e-06; norm:  8.8817e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.591926E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2882, res_abs :  1.4204e-09, res_nor :  9.9173e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.6823e-06; norm:  8.8692e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.861516E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6091e-06; norm:  8.8817e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.6823e-06; norm:  8.8692e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4554E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.257E-01 -0.121E-01  0.500E-02

 Max. velocity at interior face  0.3816E+01 ; min. -0.3974E+01
 Max. velocity at boundary face  0.7667E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415649E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@


 Write intermediate restart files
   checkpoint at iteration         48, Physical time    0.48000E-01


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

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

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

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


 Time for restart files:    0.22228E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22874E-01    5977   0.60152E-02   0.15971E+00 
c  VelocityX    0.20733E+00     388   0.59156E-01   0.33235E+01 
c  VelocityY    0.20733E+00     388   0.59156E-01   0.32679E+01 
c  VelocityZ    0.20733E+00     388   0.59156E-01   0.28001E-15 
c  Turb Kinetic 0.27983E-02     296   0.85607E-03   0.57139E-03 
c  Turb Dissipa 0.17235E+03     178   0.45872E-04   0.14542E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation          -0.032077                             7


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4553.8          2613.1         -561.29          -234.2
v  Velocity[x]                 -4.0663          4.0658       -0.015081      -0.0020521
v  Velocity[y]                 -4.1351          3.9813        0.024465           0.054
v  Velocity[z]             -1.2882e-07      3.4435e-07     -3.7623e-10     -7.6512e-11
v  Turb Kinetic Energy      7.3003e-07         0.19783       0.0042302       0.0011643
v  Turb Dissipation         4.5625e-07          7009.4           19.28          1.7585
v  Turb Viscosity           1.0818e-08        0.097302       0.0013747       0.0035025
v  CFL                       0.0033265          112.37          10.604          2.9541
v  Fourier Number            0.0013065          63.972          2.4477         0.33229


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0048592          123.27          13.052          3.2864


 TIME FOR THE TIME STEP               48:        0.64531E+01

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


 INSTANT    0.490000000E-01   TIME STEP NUMBER              49
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.8300E-08  0.1354E+00
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1097E+03 IN  0.7126E-02 -0.3100E-01  0.5000E-02
 COURANT MIN=  0.2972E-02 IN -0.4518E-02 -0.3669E-01  0.5000E-02

 FOURIER MAX=  0.7178E+02 IN  0.1392E-01 -0.1319E-01  0.5000E-02
 FOURIER MIN=  0.1305E-02 IN  0.1645E-01  0.4560E-01  0.5000E-02

 COU/FOU MAX=  0.1207E+03 IN  0.7126E-02 -0.3100E-01  0.5000E-02
 COU/FOU MIN=  0.5024E-02 IN -0.7835E-02 -0.4791E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4091e-06; norm:  5.6313e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.187466588E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884351E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 1.867203e-06, norm: 2.828420e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27271E+01 0.95812E+00
   Friction velocity        uet   :  0.52424E-04 0.33344E+00
   Friction velocity        uk    :  0.11966E-02 0.48263E+00
   Dimensionless distance   yplus :  0.88796E-01 0.12696E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        582
   Nb of faces within the viscous sub-layer     :       2209
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         49
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4090e-06; norm:  5.6316e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.874091e-06, norm: 2.823027e+06, var: Var.  2
 velocity :     258999 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   388, res_abs :  2.0498e-09, res_nor :  9.8190e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.916171e-06, norm: 2.807722e+06, var: Var.  2
 velocity :     249195 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4432E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.143146E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.4090e-06; norm:  5.6316e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.240503e-06, norm: 3.297401e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4090e-06; norm:  5.6316e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.231682E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3137, res_abs :  1.4307e-09, res_nor :  9.9946e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3010e-06; norm:  8.8575e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.574149E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2874, res_abs :  1.4191e-09, res_nor :  9.9133e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.3619e-06; norm:  8.8493e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.835634E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3010e-06; norm:  8.8575e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3619e-06; norm:  8.8493e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4567E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.259E-01 -0.121E-01  0.500E-02

 Max. velocity at interior face  0.3738E+01 ; min. -0.4118E+01
 Max. velocity at boundary face  0.7680E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415647E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23168E-01    6011   0.58376E-02   0.16185E+00 
c  VelocityX    0.20876E+00     388   0.58746E-01   0.32916E+01 
c  VelocityY    0.20876E+00     388   0.58746E-01   0.32281E+01 
c  VelocityZ    0.20876E+00     388   0.58746E-01   0.23204E-15 
c  Turb Kinetic 0.27703E-02     290   0.78940E-03   0.56799E-03 
c  Turb Dissipa 0.16625E+03     163   0.37672E-04   0.16915E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation            -4.4067                             9


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4567.4          2498.2         -584.13         -251.07
v  Velocity[x]                 -4.0379          4.0864       -0.015089      -0.0019715
v  Velocity[y]                 -4.1464          4.0273        0.021701        0.054001
v  Velocity[z]             -1.2631e-07      3.0251e-07      -3.986e-10     -8.2261e-11
v  Turb Kinetic Energy      4.7115e-07         0.17142       0.0042818       0.0011857
v  Turb Dissipation         4.6968e-07          6354.6          18.844          1.7373
v  Turb Viscosity           8.2998e-09         0.13542       0.0013805       0.0033774
v  CFL                        0.002972          109.71          10.582          2.9429
v  Fourier Number            0.0013054          71.784          2.4389         0.33231


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0050236          120.74          13.021          3.2752


 TIME FOR THE TIME STEP               49:        0.62774E+01

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


 INSTANT    0.500000000E-01   TIME STEP NUMBER              50
 ============================================================= 



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


  INITIALISATIONS                                            
  ===============                                            


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


  COMPUTATION OF PHYSICAL QUANTITIES                         
  ==================================                         

 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9982E+03  0.9982E+03
  Laminar Viscosit  0.1003E-02  0.1003E-02
  Turb Viscosity    0.1101E-07  0.9280E-01
 -----------------------------------------


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


  COMPUTATION OF CFL, FOURIER AND VARIABLE DT                
  ===========================================                


 COURANT MAX=  0.1176E+03 IN  0.1612E-01 -0.2742E-01  0.5000E-02
 COURANT MIN=  0.3106E-02 IN -0.5875E-02 -0.4827E-01  0.5000E-02

 FOURIER MAX=  0.8192E+02 IN  0.1392E-01 -0.1319E-01  0.5000E-02
 FOURIER MIN=  0.1304E-02 IN  0.1645E-01  0.4560E-01  0.5000E-02

 COU/FOU MAX=  0.1268E+03 IN  0.1612E-01 -0.2742E-01  0.5000E-02
 COU/FOU MIN=  0.4630E-02 IN -0.5875E-02 -0.4827E-01  0.5000E-02

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


  SETTING UP THE BOUNDARY CONDITIONS                         
  ==================================                         



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         380
Smooth wall               5        6813
Rough wall                6           0
Symmetry                  4      357690
Free outlet               3          11
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------

 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3939e-06; norm:  5.5981e-02


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         380        -0.714300000E-01
Smooth wall               5        6813        -0.148640893E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      357690         0.000000000E+00
Free outlet               3          11         0.713884353E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------

 _iterative_vector_gradient: isweep = 5, residue norm: 1.889974e-06, norm: 2.789243e+06, var: Var.  2

   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23910E+01 0.95523E+00
   Friction velocity        uet   :  0.12882E-04 0.33317E+00
   Friction velocity        uk    :  0.11720E-02 0.47306E+00
   Dimensionless distance   yplus :  0.17292E-01 0.12438E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        559
   Nb of faces within the viscous sub-layer     :       2193
   Total number of wall faces                   :       6813
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         50
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for          0 outlet faces on         11

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


  SOLVING NAVIER-STOKES EQUATIONS                            
  ===============================                            


   ** SOLVING VELOCITY
      ----------------

 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3937e-06; norm:  5.5986e-02
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.909975e-06, norm: 2.778797e+06, var: Var.  2
 velocity :     257672 FACES WITH UPWIND ON     352096 INTERIOR FACES 
Jacobi [velocity]:
  n_iter :   386, res_abs :  2.0269e-09, res_nor :  9.7115e-09
 velocity : CONVECTION IN   CENTERED  BLENDING WITH   0. % OF UPWIND
 _iterative_vector_gradient: isweep = 5, residue norm: 1.971147e-06, norm: 2.772388e+06, var: Var.  2
 velocity :     248534 FACES WITH UPWIND ON     352096 INTERIOR FACES 
@
@ @@ WARNING: velocity CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@

 Maximum velocity after prediction   0.4425E+01

   ** SOLVING CONTINUITY PRESSURE
      ---------------------------

 pressure         : NORMED RESIDUALS =   0.143164E+00
 _iterative_scalar_gradient; variable: pressure; converged in 5 sweeps
                             normed residual:  1.3937e-06; norm:  5.5986e-02
 _iterative_vector_gradient: isweep = 5, residue norm: 2.299466e-06, norm: 3.277138e+09, var: Var.  2
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.3937e-06; norm:  5.5986e-02
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.233394E-01, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  3162, res_abs :  1.4279e-09, res_nor :  9.9736e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.4510e-06; norm:  8.7930e-03
 pressure         : SWEEP =     1 RIGHT HAND SIDE NORM =   0.586849E-02, RELAXP =   0.100000E+01
Conjugate gradient [pressure]:
  n_iter :  2891, res_abs :  1.4313e-09, res_nor :  9.9978e-09
 _iterative_scalar_gradient; variable: Var.  0; converged in 5 sweeps
                             normed residual:  1.5431e-06; norm:  8.7989e-03
 pressure         : SWEEP =     2 RIGHT HAND SIDE NORM =   0.821362E-03, RELAXP =   0.100000E+01
@
@ @@ WARNING: pressure         PRESSURE STEP
@    ========
@  Maximum number of iterations          2 reached
@
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.4510e-06; norm:  8.7930e-03
 _iterative_scalar_gradient; variable: Var.  1; converged in 5 sweeps
                             normed residual:  1.5431e-06; norm:  8.7989e-03

 AFTER CONTINUITY PRESSURE
-------------------------------------------------------------
 Max. pressure  0.4579E+04 (max. absolute value)

 Max. velocity -0.1000E+01 en -0.710E-02 -0.303E-01  0.500E-02

 Max. velocity at interior face  0.3764E+01 ; min. -0.4312E+01
 Max. velocity at boundary face  0.7657E+00 ; min. -0.1035E+00
 Mass balance  at boundary   -0.415654E-04
-------------------------------------------------------------


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


  SOLVING TURBULENT VARIABLES EQUATIONS                      
  =====================================                      


   ** solving k-epsilon with linear prod
      ----------------------------------

@
@ @@ WARNING: k        CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@
@
@ @@ WARNING: epsilon  CONVECTION-DIFFUSION-SOURCE TERMS
@    ========
@  Maximum number of iterations          1 reached
@


 Write final restart files
   checkpoint at iteration         50, Physical time    0.50000E-01


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

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

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

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


 Time for restart files:    0.22083E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23339E-01    6053   0.57372E-02   0.16303E+00 
c  VelocityX    0.20871E+00     386   0.59476E-01   0.32332E+01 
c  VelocityY    0.20871E+00     386   0.59476E-01   0.31041E+01 
c  VelocityZ    0.20871E+00     386   0.59476E-01   0.21886E-15 
c  Turb Kinetic 0.27362E-02     283   0.81622E-03   0.58400E-03 
c  Turb Dissipa 0.15903E+03     155   0.31674E-04   0.24528E+06 
---------------------------------------------------------------
  
  

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

   field                   initial min     initial max  clips to min  clips to max
-  -------------------  --------------  --------------  ------------  ------------
a  Turb Kinetic Energy
a  Turb Dissipation           -0.03423                             7


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Pressure                    -4578.9          2346.4         -621.48         -282.55
v  Velocity[x]                 -4.0139          4.0914       -0.015614      -0.0018793
v  Velocity[y]                 -4.1663          4.0713        0.019428         0.05399
v  Velocity[z]             -1.1166e-07       2.481e-07     -4.0788e-10     -8.7846e-11
v  Turb Kinetic Energy      3.4045e-08          0.1619       0.0043664       0.0012114
v  Turb Dissipation         4.8393e-07          8616.9          18.672          1.7749
v  Turb Viscosity           1.1013e-08        0.092805       0.0013876       0.0032591
v  CFL                       0.0031055          117.61          10.586          2.9355
v  Fourier Number            0.0013044          81.917          2.4367         0.33271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0046304           126.8          13.023          3.2683


 TIME FOR THE TIME STEP               50:        0.64963E+01

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.12369E-03
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:            330.842 s
  System CPU time:            9.953 s
  Total CPU time:          1360.625 s

  Elapsed time:             341.473 s
  CPU / elapsed time          0.998

Memory use summary:

  Total memory used:                               1.315 GiB
                             local minimum:      336.324 MiB  (rank 3)
                             local maximum:      336.922 MiB  (rank 0)
  Theoretical instrumented dynamic memory:       280.355 MiB
                             local minimum:       55.695 MiB  (rank 3)
                             local maximum:       87.480 MiB  (rank 0)
