command: 
 /home/fahad/Desktop/2DCYL/CLCD/RESU/20160723-1312/cs_solver --param CLCD.xml

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

                                  (R)
                      Code_Saturne

                      Version 3.0.0


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

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


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

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

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


Local case configuration:

  Date:                Sat 23 Jul 2016 01:12:04 PM PKT
  System:              Linux 3.2.0-60-generic
  Machine:             fahad-virtual-machine
  Processor:           model name	: AMD Opteron(tm) Processor 6348
  Memory:              128943 MB
  User:                fahad (fahad)
  Directory:           /home/fahad/Desktop/2DCYL/CLCD/RESU/20160723-1312
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

  External libraries for partitioning:
    ParMETIS 3.1
    PT-SCOTCH 1.12.2147483631

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

 --- Geometry
       NPRFML =              1 (Nb max. family properties   )
       NFML   =              7 (Nb families                 )

 --- 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          )
       NPROFA =              1 (Nb internal face properties )
       NPROFB =              2 (Nb boundary face properties )


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


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

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

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

  -- Continuous phase:

       RO0    =    0.11786E+01 (Reference density           )
       VISCL0 =    0.18300E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


 ** 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)     )
       ISCALT =             -1 (Temperature salar number    )

   - Linear production k-epsilon (ITURB = 21)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (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-01 (Minimum time step           )
       DTMAX  =    0.10000E+03 (Maximum time step           )
       DTREF  =    0.10000E+00 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Pressure              0  0.1000E+01
 VelocityX             1  0.1000E+01
 VelocityY             1  0.1000E+01
 VelocityZ             1  0.1000E+01
 TurbEner              1  0.1000E+01
 Dissip                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
 TurbEner              1      1      1      1      0 0.00E+00 0.10E+01
 Dissip                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
    ------
       IVELCO =              1 (0: segregated solving of the
                                   velocity components during
                                   the prediction step
                                1: coupled solving of the
                                   velocity components       )
       IPHYDR =              0 (1: account for explicit
                                   balance between pressure
                                   gradient, gravity source
                                   terms, and head losses     )
       ICALHY =              0 (1: compute hydrastatic
                                   pressure for Dirichlet
                                   conditions for pressure
                                   on outlet                  )
       IPRCO  =              1 (1: pressure-continuity        )
       IPUCOU =              0 (1: reinforced U-P coupling    )
       NTERUP =              1 (n: n sweeps on navsto for
                                   velocity/pressure coupling )

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.10000E+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
 TurbEner            100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Dissip              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
 TurbEner              1     -1  0.1500E+01
 Dissip                1     -1  0.1500E+01
-----------------------------------

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


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


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


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


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

       NBMOMT =              0 (Number of moments           )

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


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

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

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


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


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

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

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


  Multigrid coarsening type: algebraic, face traveral by criteria

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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =             10 (Final time step required    )

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


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


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

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

 --- Post-processed variables

       Number Name
         2 Pressure        
         3 VelocityX       
         4 VelocityY       
         5 VelocityZ       
         6 TurbEner        
         7 Dissip          
        10 TurbVisc        
        11 CourantNb       
        12 FourierNb       
        13 total_pressure  
         --           --

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

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

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

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

         2 Pressure                       0
         3 VelocityX                      0
         4 VelocityY                      0
         5 VelocityZ                      0
         6 TurbEner                       0
         7 Dissip                         0
        10 TurbVisc                    -999
        11 CourantNb                   -999
        12 FourierNb                   -999
        13 total_pressure              -999
         --           --                --

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


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


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

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


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


 Reading file:        mesh_input
 Finished reading:    mesh_input


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: every 1 time steps

 Number of cells:                                      8000

 ----------------------------------------------------------
 Number of cells + halo cells:                         8000


 ----------------------------------------------------------
 Number of interior faces:                             15800

 ----------------------------------------------------------
 Number of boundary faces:                             16400

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =          2
      2 : [          3 ;          4 ] =       7998

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

 Renumbering mesh:

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


 Matrix bandwidth for volume mesh :          4839
 Matrix profile/lines for volume mesh :      180

 Mesh coordinates:               minimum    and maximum
                       X : -1.0000000e+01  4.0000000e+01
                       Y : -1.0000000e+01  1.0000000e+01
                       Z :  0.0000000e+00  1.0000000e+00
 Mesh
     Number of cells:          8000
     Number of interior faces: 15800
     Number of boundary faces: 16400
     Number of vertices:       16400

 Groups:
    "bottom"
       boundary faces:           80
    "cylinderwalls"
       boundary faces:          160
    "frontAndback"
       boundary faces:        16000
    "inlet"
       boundary faces:           40
    "outlet"
       boundary faces:           40
    "top"
       boundary faces:           80

 --- Information on the volumes
       Minimum control volume      =  3.1736252e-04
       Maximum control volume      =  4.6574743e-01
       Total volume for the domain =  9.9921480e+02

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

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 0 -->   0 %

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

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

 Computing geometric quantities (0.0192 s)
                                                             
       ALMAX  =    0.99744E+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
  TurbEner          0.6000E-03  0.6000E-03
  Dissip            0.1326E-06  0.1326E-06
 ---------------------------------

  Local Time Step   0.1000E+00  0.1000E+00
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  Density           0.1179E+01  0.1179E+01
  LamVisc           0.1830E-04  0.1830E-04
  TurbVisc          0.2880E+00  0.2880E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          40
Smooth wall               5           0
Rough wall                6         160
Symmetry                  4       16160
Free outlet               3          40
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.40000E+02   0.25000E+00   0.50000E+00



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55543E-12 0.71396E-12
   Friction velocity        uk    :  0.13416E-01 0.13416E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.36040E+01     592   0.41298E+00   0.99467E+00 
c  VelocityX    0.19588E+01      17   0.16436E-01   0.90061E+01 
c  VelocityY    0.19588E+01      17   0.16436E-01   0.31837E-01 
c  VelocityZ    0.19588E+01      17   0.16436E-01   0.10009E-27 
c  TurbEner     0.14447E+00     121   0.33901E-02   0.24089E-06 
c  Dissip       0.15923E-01    1394   0.97447E-02   0.51200E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure     0.44198E+01   0.56364E+03         --         -- 
v  VelocityX    0.32398E-01   0.22196E+01         --         -- 
v  VelocityY   -0.10531E+01   0.10531E+01         --         -- 
v  VelocityZ   -0.17997E-13   0.19562E-13         --         -- 
v  TurbEner     0.59999E-03   0.18475E-02          0          0 
v  Dissip       0.13261E-06   0.33734E-02          0          0 
v  TurbVisc     0.28796E+00   0.28796E+00          0          0 
v  CourantNb    0.00000E+00   0.00000E+00          0          0 
v  FourierNb    0.14117E+00   0.26954E+03          0          0 
v  total_pressu 0.10133E+06   0.10189E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.59999E-03   0.18475E-02          0          0 
a  Dissip       0.13261E-06   0.33734E-02          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.39625E+02  0.97500E+01  0.50000E+00  
Courant max  0.00000E+00  0.39625E+02  0.97500E+01  0.50000E+00  
Fourier min  0.14117E+00  0.39625E+02 -0.97500E+01  0.50000E+00  
Fourier max  0.26954E+03 -0.52454E+00  0.10443E-01  0.50000E+00  
Cou_Fou min  0.14117E+00  0.39625E+02 -0.97500E+01  0.50000E+00  
Cou_Fou max  0.26954E+03 -0.52454E+00  0.10443E-01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                1:        0.37070E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235724006E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.21441E+01
   Friction velocity        uet   :  0.27721E-01 0.15850E+01
   Friction velocity        uk    :  0.13416E-01 0.13416E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15684E+01     449   0.24278E+00   0.99787E+00 
c  VelocityX    0.20289E+03     105   0.81166E-03   0.55389E-01 
c  VelocityY    0.20289E+03     105   0.81166E-03   0.85636E-02 
c  VelocityZ    0.20289E+03     105   0.81166E-03   0.18518E-28 
c  TurbEner     0.15740E+00      85   0.61744E-04   0.85709E-07 
c  Dissip       0.25512E-01      58   0.27812E-04   0.21997E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.20782E+01   0.28161E+02         --         -- 
v  VelocityX    0.18971E-01   0.17962E+01         --         -- 
v  VelocityY   -0.95893E+00   0.95893E+00         --         -- 
v  VelocityZ   -0.94734E-14   0.16022E-13         --         -- 
v  TurbEner     0.43220E-03   0.25041E-02          0          0 
v  Dissip       0.13102E-06   0.98398E-02          0          0 
v  TurbVisc     0.11320E-04   0.28796E+00          0          0 
v  CourantNb    0.99897E-01   0.11091E+02          0          0 
v  FourierNb    0.87923E-03   0.13582E+02          0          0 
v  total_pressu 0.10132E+06   0.10135E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.43220E-03   0.25041E-02          0          0 
a  Dissip       0.13102E-06   0.98398E-02          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.99897E-01  0.95260E+01 -0.23810E+00  0.50000E+00  
Courant max  0.11091E+02 -0.30046E-01  0.50704E+00  0.50000E+00  
Fourier min  0.87923E-03 -0.95260E+01  0.23810E+00  0.50000E+00  
Fourier max  0.13582E+02 -0.14722E+01  0.14314E+01  0.50000E+00  
Cou_Fou min  0.10990E+00 -0.95260E+01  0.23810E+00  0.50000E+00  
Cou_Fou max  0.15579E+02 -0.14722E+01  0.14314E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                2:        0.26175E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235723998E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.16643E+01
   Friction velocity        uet   :  0.16268E-01 0.12537E+01
   Friction velocity        uk    :  0.11387E-01 0.23436E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63835E+00     521   0.17211E+00   0.73343E+00 
c  VelocityX    0.21801E+03     119   0.76063E-03   0.11145E-01 
c  VelocityY    0.21801E+03     119   0.76063E-03   0.44348E-02 
c  VelocityZ    0.21801E+03     119   0.76063E-03   0.48611E-29 
c  TurbEner     0.17200E+00      74   0.18855E-04   0.63395E-07 
c  Dissip       0.34061E-01      57   0.14082E-04   0.18173E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.16564E+01   0.13671E+02         --         -- 
v  VelocityX    0.15915E-01   0.17562E+01         --         -- 
v  VelocityY   -0.96032E+00   0.96032E+00         --         -- 
v  VelocityZ   -0.69870E-14   0.13432E-13         --         -- 
v  TurbEner     0.31886E-03   0.33006E-02          0          0 
v  Dissip       0.13069E-06   0.17675E-01          0          0 
v  TurbVisc     0.10467E-04   0.29105E+00          0          0 
v  CourantNb    0.10672E+00   0.89245E+01          0          0 
v  FourierNb    0.98664E-03   0.14244E+02          0          0 
v  total_pressu 0.10132E+06   0.10134E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.31886E-03   0.33006E-02          0          0 
a  Dissip       0.13069E-06   0.17675E-01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.10672E+00  0.95260E+01  0.23810E+00  0.50000E+00  
Courant max  0.89245E+01 -0.89728E-01 -0.50012E+00  0.50000E+00  
Fourier min  0.98664E-03 -0.95260E+01 -0.23810E+00  0.50000E+00  
Fourier max  0.14244E+02 -0.14722E+01  0.14314E+01  0.50000E+00  
Cou_Fou min  0.11001E+00 -0.95260E+01 -0.23810E+00  0.50000E+00  
Cou_Fou max  0.16171E+02 -0.14722E+01  0.14314E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                3:        0.29088E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235723999E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.15018E+01
   Friction velocity        uet   :  0.10362E-01 0.11293E+01
   Friction velocity        uk    :  0.97805E-02 0.31467E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59632E+00     521   0.34904E+00   0.11352E+01 
c  VelocityX    0.21683E+03      95   0.57358E-03   0.92450E-03 
c  VelocityY    0.21683E+03      95   0.57358E-03   0.40347E-03 
c  VelocityZ    0.21683E+03      95   0.57358E-03   0.17399E-29 
c  TurbEner     0.18594E+00      87   0.19958E-04   0.49703E-07 
c  Dissip       0.41232E-01      56   0.86508E-05   0.20692E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.19014E+01   0.20455E+01         --         -- 
v  VelocityX    0.10935E-01   0.17801E+01         --         -- 
v  VelocityY   -0.97993E+00   0.97993E+00         --         -- 
v  VelocityZ   -0.60376E-14   0.11377E-13         --         -- 
v  TurbEner     0.24693E-03   0.51649E-02          0          0 
v  Dissip       0.13102E-06   0.27459E-01          0          0 
v  TurbVisc     0.97700E-05   0.29078E+00          0          0 
v  CourantNb    0.10902E+00   0.85768E+01          0          0 
v  FourierNb    0.89055E-03   0.14436E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.24693E-03   0.51649E-02          0          0 
a  Dissip       0.13102E-06   0.27459E-01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.10902E+00 -0.95260E+01  0.23810E+00  0.50000E+00  
Courant max  0.85768E+01 -0.72892E-01 -0.51993E+00  0.50000E+00  
Fourier min  0.89055E-03 -0.86092E+01  0.21491E+00  0.50000E+00  
Fourier max  0.14436E+02 -0.14722E+01  0.14314E+01  0.50000E+00  
Cou_Fou min  0.11014E+00 -0.95260E+01  0.23810E+00  0.50000E+00  
Cou_Fou max  0.16333E+02 -0.14722E+01  0.14314E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                4:        0.28048E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235724001E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.14173E+01
   Friction velocity        uet   :  0.74815E-02 0.10674E+01
   Friction velocity        uk    :  0.86070E-02 0.39363E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.35288E+00     486   0.26943E+00   0.90727E+00 
c  VelocityX    0.21396E+03     104   0.41591E-03   0.65341E-03 
c  VelocityY    0.21396E+03     104   0.41591E-03   0.12143E-03 
c  VelocityZ    0.21396E+03     104   0.41591E-03   0.75572E-30 
c  TurbEner     0.19905E+00      87   0.14444E-04   0.41319E-07 
c  Dissip       0.47387E-01      56   0.61299E-05   0.31303E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.25476E+01   0.28872E+00         --         -- 
v  VelocityX    0.20422E-02   0.18016E+01         --         -- 
v  VelocityY   -0.99507E+00   0.99507E+00         --         -- 
v  VelocityZ   -0.53586E-14   0.96308E-14         --         -- 
v  TurbEner     0.19647E-03   0.76388E-02          0          0 
v  Dissip       0.13149E-06   0.40552E-01          0          0 
v  TurbVisc     0.92745E-05   0.29016E+00          0          0 
v  CourantNb    0.10902E+00   0.87352E+01          0          0 
v  FourierNb    0.87731E-03   0.14881E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.19647E-03   0.76388E-02          0          0 
a  Dissip       0.13149E-06   0.40552E-01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.10902E+00 -0.95260E+01  0.23810E+00  0.50000E+00  
Courant max  0.87352E+01 -0.52142E-01 -0.52224E+00  0.50000E+00  
Fourier min  0.87731E-03 -0.86092E+01  0.21491E+00  0.50000E+00  
Fourier max  0.14881E+02 -0.13465E+01  0.13088E+01  0.50000E+00  
Cou_Fou min  0.11027E+00 -0.95260E+01  0.23810E+00  0.50000E+00  
Cou_Fou max  0.16949E+02 -0.13465E+01  0.13088E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                5:        0.27825E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235724001E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.13751E+01
   Friction velocity        uet   :  0.26894E-03 0.10187E+01
   Friction velocity        uk    :  0.76773E-02 0.47871E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.16218E+00     431   0.12245E+00   0.54659E+00 
c  VelocityX    0.21280E+03      88   0.23936E-03   0.32150E-03 
c  VelocityY    0.21280E+03      88   0.23936E-03   0.84063E-04 
c  VelocityZ    0.21280E+03      88   0.23936E-03   0.37882E-30 
c  TurbEner     0.21128E+00      87   0.84495E-05   0.36036E-07 
c  Dissip       0.52764E-01      56   0.49088E-05   0.53270E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.20312E+01   0.32985E+00         --         -- 
v  VelocityX   -0.71992E-02   0.18172E+01         --         -- 
v  VelocityY   -0.10071E+01   0.10071E+01         --         -- 
v  VelocityZ   -0.47598E-14   0.81768E-14         --         -- 
v  TurbEner     0.16003E-03   0.10917E-01          0          0 
v  Dissip       0.13181E-06   0.58370E-01          0          0 
v  TurbVisc     0.88325E-05   0.28973E+00          0          0 
v  CourantNb    0.19545E-01   0.88256E+01          0          0 
v  FourierNb    0.91287E-03   0.15371E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.16003E-03   0.10917E-01          0          0 
a  Dissip       0.13181E-06   0.58370E-01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.19545E-01  0.50781E+00 -0.10020E-01  0.50000E+00  
Courant max  0.88256E+01 -0.52142E-01 -0.52224E+00  0.50000E+00  
Fourier min  0.91287E-03 -0.86092E+01  0.21491E+00  0.50000E+00  
Fourier max  0.15371E+02 -0.13465E+01  0.13088E+01  0.50000E+00  
Cou_Fou min  0.40316E-01  0.50781E+00 -0.10020E-01  0.50000E+00  
Cou_Fou max  0.17444E+02 -0.13465E+01  0.13088E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                6:        0.26087E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235724000E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.13520E+01
   Friction velocity        uet   :  0.95449E-04 0.98989E+00
   Friction velocity        uk    :  0.69288E-02 0.57229E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.94492E-01     468   0.83625E-01   0.41338E+00 
c  VelocityX    0.21277E+03      91   0.13482E-03   0.14066E-03 
c  VelocityY    0.21277E+03      91   0.13482E-03   0.19435E-04 
c  VelocityZ    0.21277E+03      91   0.13482E-03   0.21277E-30 
c  TurbEner     0.22264E+00      89   0.55099E-05   0.32898E-07 
c  Dissip       0.57530E-01      56   0.46502E-05   0.92769E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.16473E+01   0.70388E+00         --         -- 
v  VelocityX   -0.83609E-01   0.18277E+01         --         -- 
v  VelocityY   -0.10100E+01   0.10100E+01         --         -- 
v  VelocityZ   -0.42196E-14   0.69725E-14         --         -- 
v  TurbEner     0.13665E-03   0.15207E-01          0          0 
v  Dissip       0.13202E-06   0.81849E-01          0          0 
v  TurbVisc     0.85065E-05   0.28952E+00          0          0 
v  CourantNb    0.65260E-01   0.88493E+01          0          0 
v  FourierNb    0.97150E-03   0.15758E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.13665E-03   0.15207E-01          0          0 
a  Dissip       0.13202E-06   0.81849E-01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.65260E-01  0.50781E+00  0.10020E-01  0.50000E+00  
Courant max  0.88493E+01 -0.72892E-01 -0.51993E+00  0.50000E+00  
Fourier min  0.97150E-03 -0.86092E+01  0.21491E+00  0.50000E+00  
Fourier max  0.15758E+02 -0.13465E+01  0.13088E+01  0.50000E+00  
Cou_Fou min  0.85799E-01  0.50781E+00  0.10020E-01  0.50000E+00  
Cou_Fou max  0.17830E+02 -0.13465E+01  0.13088E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                7:        0.26896E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235724000E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.13367E+01
   Friction velocity        uet   :  0.81993E-02 0.97165E+00
   Friction velocity        uk    :  0.64027E-02 0.67544E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68227E-01     447   0.82300E-01   0.36231E+00 
c  VelocityX    0.21302E+03      74   0.11574E-03   0.87585E-04 
c  VelocityY    0.21302E+03      74   0.11574E-03   0.14391E-04 
c  VelocityZ    0.21302E+03      74   0.11574E-03   0.12866E-30 
c  TurbEner     0.23316E+00      92   0.44255E-05   0.31540E-07 
c  Dissip       0.61822E-01      55   0.61877E-05   0.15817E-06 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.15454E+01   0.81298E+00         --         -- 
v  VelocityX   -0.21293E+00   0.18338E+01         --         -- 
v  VelocityY   -0.10138E+01   0.10138E+01         --         -- 
v  VelocityZ   -0.37388E-14   0.59494E-14         --         -- 
v  TurbEner     0.12338E-03   0.20740E-01          0          0 
v  Dissip       0.13218E-06   0.11374E+00          0          0 
v  TurbVisc     0.84045E-05   0.28937E+00          0          0 
v  CourantNb    0.79875E-01   0.88622E+01          0          0 
v  FourierNb    0.10422E-02   0.16225E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.12338E-03   0.20740E-01          0          0 
a  Dissip       0.13218E-06   0.11374E+00          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.79875E-01  0.54313E+00 -0.10914E-01  0.50000E+00  
Courant max  0.88622E+01 -0.72892E-01 -0.51993E+00  0.50000E+00  
Fourier min  0.10422E-02 -0.86092E+01  0.21491E+00  0.50000E+00  
Fourier max  0.16225E+02 -0.12334E+01  0.11985E+01  0.50000E+00  
Cou_Fou min  0.10407E+00  0.54313E+00 -0.10914E-01  0.50000E+00  
Cou_Fou max  0.18474E+02 -0.12334E+01  0.11985E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                8:        0.25783E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235724000E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.13238E+01
   Friction velocity        uet   :  0.12041E-01 0.95981E+00
   Friction velocity        uk    :  0.60839E-02 0.78879E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.44152E-01     394   0.41118E-01   0.27194E+00 
c  VelocityX    0.21322E+03      92   0.15649E-03   0.62032E-04 
c  VelocityY    0.21322E+03      92   0.15649E-03   0.17002E-04 
c  VelocityZ    0.21322E+03      92   0.15649E-03   0.85802E-31 
c  TurbEner     0.24287E+00      94   0.38291E-05   0.31723E-07 
c  Dissip       0.65777E-01      55   0.10855E-04   0.25593E-06 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.15551E+01   0.81182E+00         --         -- 
v  VelocityX   -0.32359E+00   0.18347E+01         --         -- 
v  VelocityY   -0.10165E+01   0.10165E+01         --         -- 
v  VelocityZ   -0.33057E-14   0.50787E-14         --         -- 
v  TurbEner     0.11737E-03   0.27622E-01          0          0 
v  Dissip       0.13223E-06   0.15526E+00          0          0 
v  TurbVisc     0.85454E-05   0.28929E+00          0          0 
v  CourantNb    0.10884E+00   0.88868E+01          0          0 
v  FourierNb    0.10619E-02   0.16864E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.11737E-03   0.27622E-01          0          0 
a  Dissip       0.13223E-06   0.15526E+00          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.10884E+00  0.95260E+01  0.23810E+00  0.50000E+00  
Courant max  0.88868E+01 -0.93537E-01 -0.51687E+00  0.50000E+00  
Fourier min  0.10619E-02 -0.77840E+01  0.19404E+00  0.50000E+00  
Fourier max  0.16864E+02 -0.12334E+01  0.11985E+01  0.50000E+00  
Cou_Fou min  0.11068E+00 -0.95260E+01  0.23810E+00  0.50000E+00  
Cou_Fou max  0.19112E+02 -0.12334E+01  0.11985E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                9:        0.25805E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          40        -0.235724000E+02
Smooth wall               5           0         0.000000000E+00
Rough wall                6         160         0.000000000E+00
Symmetry                  4       16160         0.000000000E+00
Free outlet               3          40         0.235724000E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.13112E+01
   Friction velocity        uet   :  0.14772E-01 0.94970E+00
   Friction velocity        uk    :  0.59339E-02 0.91031E-01
   Rough dimensionless dist yplus :  0.80087E+00 0.11301E+01
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------




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


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

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

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

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


 Time for restart files:    0.95530E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.29205E-01     396   0.16528E-01   0.20322E+00 
c  VelocityX    0.21331E+03      95   0.11839E-03   0.46006E-04 
c  VelocityY    0.21331E+03      95   0.11839E-03   0.15989E-04 
c  VelocityZ    0.21331E+03      95   0.11839E-03   0.60006E-31 
c  TurbEner     0.25186E+00      97   0.35453E-05   0.33193E-07 
c  Dissip       0.69530E-01      55   0.19521E-04   0.38692E-06 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.15621E+01   0.81134E+00         --         -- 
v  VelocityX   -0.39667E+00   0.18345E+01         --         -- 
v  VelocityY   -0.10199E+01   0.10199E+01         --         -- 
v  VelocityZ   -0.31944E-14   0.46519E-14         --         -- 
v  TurbEner     0.11704E-03   0.35677E-01          0          0 
v  Dissip       0.13227E-06   0.20869E+00          0          0 
v  TurbVisc     0.89267E-05   0.28923E+00          0          0 
v  CourantNb    0.10887E+00   0.88877E+01          0          0 
v  FourierNb    0.10813E-02   0.17409E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.11704E-03   0.35677E-01          0          0 
a  Dissip       0.13227E-06   0.20869E+00          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.10887E+00  0.95260E+01  0.23810E+00  0.50000E+00  
Courant max  0.88877E+01 -0.11405E+00 -0.51304E+00  0.50000E+00  
Fourier min  0.10813E-02 -0.77840E+01  0.19404E+00  0.50000E+00  
Fourier max  0.17409E+02 -0.12334E+01  0.11985E+01  0.50000E+00  
Cou_Fou min  0.11076E+00 -0.95260E+01  0.23810E+00  0.50000E+00  
Cou_Fou max  0.19681E+02 -0.11316E+01  0.10991E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               10:        0.26639E+00

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.10870E-02
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:              2.760 s
  System CPU time:            0.092 s

  Elapsed time:               2.848 s
  CPU / elapsed time          1.001

Memory use summary:

  Total memory used:                             122.332 MiB
  Theoretical instrumented dynamic memory:         8.527 MiB
