command: 
 ./cs_solver --param Calc

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

                                  (R)
                      Code_Saturne

                      Version 3.2.1


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

  build Fr 13 Dez 2013 14:02:19 CET
  MPI version 2.2 (MPICH2 1.4.1)


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

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

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


Local case configuration:

  Date:                Sa 21 Dez 2013 10:45:13 CET
  System:              Linux 3.8.0-30-generic
  Machine:             caelinux-VirtualBox
  Processor:           model name	: Intel(R) Core(TM) i7-2675QM CPU @ 2.20GHz
  Memory:              8376 MB
  User:                caelinux (caelinux)
  Directory:           /home/caelinux/opt/code_saturne-3.2.1/arch/Linux_x86_64/bin/TUBE/Case1/RESU/20131221-1045
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

  External libraries for partitioning:
    METIS

 Reading metadata from file: "mesh_input/mesh_01"
 Reading metadata from file: "mesh_input/mesh_02"

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

                   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    =    0.10350E+04 (Reference density           )
       VISCL0 =    0.35000E-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  =             20 (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)     )

   - k-epsilon           (ITURB = 20)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              1 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )


   - 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))

   - k-epsilon           (ITURB = 20)
       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
    ------
       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 =            100 (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  =              8 (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)


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


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

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

 Number of cells:                                      8066

 ----------------------------------------------------------
 Number of cells + halo cells:                         8066


 ----------------------------------------------------------
 Number of interior faces:                             14140

 ----------------------------------------------------------
 Number of boundary faces:                             3984

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =         56
      2 : [          3 ;          4 ] =       8010

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

 Writing file:        mesh_output
 Finished writing:    mesh_output

 Renumbering mesh:

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


 Matrix bandwidth for volume mesh :          4740
 Matrix profile/lines for volume mesh :      2163

 Mesh coordinates:               minimum    and maximum
                       X : -1.4999917e+01  1.5000000e+01
                       Y : -1.4999991e+01  1.4998067e+01
                       Z :  0.0000000e+00  1.0000000e+02
 Mesh
     Number of cells:          8066
     Number of interior faces: 14140
     Number of boundary faces: 3984
     Number of vertices:       2356

 Groups:
    "boundary"
       boundary faces:         2052
    "inlet"
       boundary faces:           52
    "outlet"
       boundary faces:           48
    "rotor_wall"
       boundary faces:          974
    "stator_wall"
       boundary faces:          858

 --- Information on the volumes
       Minimum control volume      =  8.8218868e-01
       Maximum control volume      =  4.0697888e+01
       Total volume for the domain =  6.5084821e+04

  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: 490 -->   6 %

  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 (0.0185 s)
                                                             
       ALMAX  =    0.40076E+02 (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            0.3301E-07  0.3301E-07
 ---------------------------------

  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           0.1035E+04  0.1035E+04
  LamVisc           0.3500E-02  0.3500E-02
  TurbVisc          0.1016E+04  0.1016E+04
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          52
Smooth wall               5        1832
Rough wall                6           0
Symmetry                  4        2052
Free outlet               3          48
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =   -0.14151E+01   0.64080E+00   0.00000E+00



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52         0.000000000E+00
Smooth wall               5        1832         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.13416E-01 0.13416E-01
   Dimensionless distance   yplus :  0.14572E+04 0.65476E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.45246E+06     581   0.35052E+00   0.93160E+00 
c  VelocityX    0.51469E+06      10   0.23110E-01   0.35294E+01 
c  VelocityY    0.51469E+06      10   0.23110E-01   0.36776E+01 
c  VelocityZ    0.51469E+06      10   0.23110E-01   0.42249E+03 
c  TurbEner     0.22550E+07      23   0.13134E-01   0.19366E+00 
c  Dissip       0.72638E+06      23   0.11802E-01   0.21800E-01 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0801e-06                          1064


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                     0      8.5695e+06      1.7594e+06       2.969e+06
v  Velocity[x]            -5.9221          6.3606       0.0086514        0.012586
v  Velocity[y]            -7.6669          7.0628       -0.005368       0.0015372
v  Velocity[z]            -10.742         0.43929         -3.0654         -5.1618
v  TurbEner            0.00059832          2.0968        0.010854        0.022616
v  Dissip              1.9614e-10          1.1084       0.0031212        0.006308
v  TurbVisc                  1016            1016            1016            1016
v  CourantNb                    0               0               0               0
v  FourierNb             0.065204           1.382          0.3159         0.22663
v  total_pressure      1.0132e+05      8.6709e+06      1.8607e+06      3.0703e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.065204           1.382          0.3159         0.22663


 TIME FOR THE TIME STEP                1:        0.27214E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.134307287E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393708E+07
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 0.77925E+01
   Friction velocity        uet   :  0.00000E+00 0.37328E+00
   Friction velocity        uk    :  0.13398E-01 0.57219E+00
   Dimensionless distance   yplus :  0.14556E+04 0.21846E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28459E+06     482   0.51583E-01   0.11604E+01 
c  VelocityX    0.66357E+08      40   0.21103E-01   0.25819E+00 
c  VelocityY    0.66357E+08      40   0.21103E-01   0.25661E+00 
c  VelocityZ    0.66357E+08      40   0.21103E-01   0.83744E+00 
c  TurbEner     0.42622E+07      48   0.23245E-01   0.29295E+00 
c  Dissip       0.77640E+06      44   0.91108E-02   0.40852E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.1327e-06                           448


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -31141      2.4249e+05           29957           51336
v  Velocity[x]            -5.9016          5.5125       0.0012871      0.00054518
v  Velocity[y]            -7.6797          6.2468      -0.0080706     -0.00073238
v  Velocity[z]            -10.305         0.76021         -3.1444         -5.2986
v  TurbEner            0.00059607          6.3907        0.031501        0.052928
v  Dissip              1.3633e-10         0.99414       0.0058727        0.010937
v  TurbVisc               0.52086      1.7097e+05          847.07          803.36
v  CourantNb                    0          2.8412         0.28212         0.45206
v  FourierNb           9.2274e-05          23.006         0.24833         0.19466
v  total_pressure           70184      3.4381e+05      1.3128e+05      1.5266e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022892          23.006         0.53045         0.64672


 TIME FOR THE TIME STEP                2:        0.24779E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.785482029E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.80692E+01
   Friction velocity        uet   :  0.00000E+00 0.35077E+00
   Friction velocity        uk    :  0.13372E-01 0.10078E+01
   Dimensionless distance   yplus :  0.14534E+04 0.39154E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12974E+06     488   0.31269E-01   0.58432E+00 
c  VelocityX    0.69745E+08      21   0.18348E-01   0.12200E+00 
c  VelocityY    0.69745E+08      21   0.18348E-01   0.11714E+00 
c  VelocityZ    0.69745E+08      21   0.18348E-01   0.19388E+00 
c  TurbEner     0.27604E+07      24   0.23667E-01   0.56234E-01 
c  Dissip       0.84697E+06      42   0.14014E-01   0.62215E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip          -0.02853                           434


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -48398           58168         -3491.7         -5223.2
v  Velocity[x]            -6.2507          5.6991      -0.0004716      -0.0021585
v  Velocity[y]            -7.8123          6.3251      -0.0090489      -0.0012373
v  Velocity[z]            -10.205           0.349         -3.1545         -5.3193
v  TurbEner            0.00059382          4.7145        0.039119        0.064318
v  Dissip              6.9879e-14          1.0833       0.0080655        0.014498
v  TurbVisc               0.54607      2.4597e+05          801.96          658.06
v  CourantNb                    0          2.8549         0.28143         0.45111
v  FourierNb           7.3988e-05          33.497         0.25896         0.17793
v  total_pressure           52927      1.5949e+05           97833           96102


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022891          33.497         0.54039         0.62905


 TIME FOR THE TIME STEP                3:        0.24654E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.246374951E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393702E+07
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 0.79696E+01
   Friction velocity        uet   :  0.00000E+00 0.34570E+00
   Friction velocity        uk    :  0.13347E-01 0.88643E+00
   Dimensionless distance   yplus :  0.14511E+04 0.34439E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.84792E+05     418   0.14434E-01   0.36110E+00 
c  VelocityX    0.68572E+08      19   0.16510E-01   0.65692E-01 
c  VelocityY    0.68572E+08      19   0.16510E-01   0.73034E-01 
c  VelocityZ    0.68572E+08      19   0.16510E-01   0.10351E+00 
c  TurbEner     0.25589E+07   10000   0.44072E-02   0.32861E-01 
c  Dissip       0.75957E+06   10000   0.24838E-02   0.27884E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -4.5273e-05                           392


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -73974           38197         -5785.6         -9112.3
v  Velocity[x]            -6.4865          5.8754      -0.0012128      -0.0033928
v  Velocity[y]            -7.9796           6.385      -0.0095979      -0.0012569
v  Velocity[z]            -10.282         0.17105         -3.1564         -5.3262
v  TurbEner            0.00059157          3.9517        0.044916        0.072716
v  Dissip              1.0931e-10         0.94567       0.0098113        0.017008
v  TurbVisc               0.54512      4.7988e+08           61088           59208
v  CourantNb                    0          2.8645         0.28104         0.45093
v  FourierNb           8.8772e-05           40395          10.396          10.118
v  total_pressure           27351      1.3952e+05           95539           92213


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022889           40395          10.677          10.569


 TIME FOR THE TIME STEP                4:        0.16184E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.423542209E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393702E+07
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 0.79856E+01
   Friction velocity        uet   :  0.00000E+00 0.33802E+00
   Friction velocity        uk    :  0.13322E-01 0.74506E+00
   Dimensionless distance   yplus :  0.14489E+04 0.28947E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57705E+05     362   0.85221E-02   0.23152E+00 
c  VelocityX    0.68530E+08      19   0.14990E-01   0.46887E-01 
c  VelocityY    0.68530E+08      19   0.14990E-01   0.48987E-01 
c  VelocityZ    0.68530E+08      19   0.14990E-01   0.72588E-01 
c  TurbEner     0.25575E+07      23   0.23735E-02   0.23663E-01 
c  Dissip       0.74223E+06      40   0.14881E-02   0.24986E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00017505                           371


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -78286           41230         -5358.5         -8379.5
v  Velocity[x]            -6.4668          6.0217      -0.0016603      -0.0040627
v  Velocity[y]            -8.1178          6.4353       -0.010103      -0.0012808
v  Velocity[z]            -10.311         0.34367         -3.1582         -5.3319
v  TurbEner            0.00058929          4.0781        0.050095        0.080112
v  Dissip              6.2945e-11          1.4109        0.011555        0.019367
v  TurbVisc               0.60053      3.0679e+05          863.47           623.3
v  CourantNb                    0          2.8631         0.28063          0.4507
v  FourierNb           0.00010692          50.929         0.27661         0.17446
v  total_pressure           23039      1.4255e+05           95967           92946


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022887          50.929         0.55725         0.62516


 TIME FOR THE TIME STEP                5:        0.22313E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.465166109E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.79976E+01
   Friction velocity        uet   :  0.00000E+00 0.33542E+00
   Friction velocity        uk    :  0.13296E-01 0.74038E+00
   Dimensionless distance   yplus :  0.14467E+04 0.24253E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.43012E+05     328   0.60328E-02   0.16665E+00 
c  VelocityX    0.68655E+08      19   0.14064E-01   0.32966E-01 
c  VelocityY    0.68655E+08      19   0.14064E-01   0.31839E-01 
c  VelocityZ    0.68655E+08      19   0.14064E-01   0.54122E-01 
c  TurbEner     0.26222E+07      72   0.15266E-02   0.18457E-01 
c  Dissip       0.75885E+06     103   0.11995E-02   0.24588E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.2912e-05                           374


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -81196           42103         -5454.5         -8541.3
v  Velocity[x]            -6.5161          6.1453       -0.002194      -0.0047663
v  Velocity[y]            -8.1826          6.4116      -0.0099975     -0.00070195
v  Velocity[z]            -10.266         0.61005         -3.1593         -5.3362
v  TurbEner            0.00058704            4.52        0.054924        0.086973
v  Dissip               1.047e-12          1.9765         0.01336        0.021727
v  TurbVisc               0.71304      5.3276e+05          1130.4          871.97
v  CourantNb                    0          2.8679         0.28023         0.45046
v  FourierNb           0.00013183          70.294         0.35791         0.23742
v  total_pressure           20129      1.4343e+05           95870           92784


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022884          70.294         0.63814         0.68788


 TIME FOR THE TIME STEP                6:        0.21264E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.222524286E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.80169E+01
   Friction velocity        uet   :  0.00000E+00 0.33311E+00
   Friction velocity        uk    :  0.13271E-01 0.72544E+00
   Dimensionless distance   yplus :  0.14445E+04 0.20273E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.36296E+05     316   0.44908E-02   0.13588E+00 
c  VelocityX    0.68759E+08      35   0.14487E-01   0.26603E-01 
c  VelocityY    0.68759E+08      35   0.14487E-01   0.25457E-01 
c  VelocityZ    0.68759E+08      35   0.14487E-01   0.43929E-01 
c  TurbEner     0.27289E+07    9837   0.27986E-02   0.15305E-01 
c  Dissip       0.80222E+06   10000   0.15941E-02   0.25547E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0044177                           348


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -82057           41695         -5646.8         -8857.2
v  Velocity[x]            -6.5135          6.2551      -0.0026097      -0.0051126
v  Velocity[y]            -8.1899          6.4876       -0.010057     -0.00047713
v  Velocity[z]            -10.274         0.78279           -3.16         -5.3391
v  TurbEner            0.00058479          5.2659        0.059599        0.093634
v  Dissip               2.684e-11          2.6403        0.015245        0.024154
v  TurbVisc               0.80843      3.2028e+07          5209.1          3906.7
v  CourantNb                    0          2.8707         0.27989         0.45023
v  FourierNb           0.00014819          5239.1          1.8866          1.2483
v  total_pressure           19268      1.4302e+05           95678           92468


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022881          5239.1          2.1665          1.6986


 TIME FOR THE TIME STEP                7:        0.15149E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.499641988E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.80267E+01
   Friction velocity        uet   :  0.00000E+00 0.33193E+00
   Friction velocity        uk    :  0.13245E-01 0.69933E+00
   Dimensionless distance   yplus :  0.14423E+04 0.18069E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.32619E+05     291   0.34703E-02   0.11895E+00 
c  VelocityX    0.68846E+08      35   0.14167E-01   0.20912E-01 
c  VelocityY    0.68846E+08      35   0.14167E-01   0.21579E-01 
c  VelocityZ    0.68846E+08      35   0.14167E-01   0.40913E-01 
c  TurbEner     0.28606E+07      61   0.86955E-03   0.12856E-01 
c  Dissip       0.86476E+06      74   0.94715E-03   0.27138E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -5.9624e-07                           351


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -83303           41237         -5675.4         -8908.7
v  Velocity[x]            -6.5907          6.3474      -0.0029605      -0.0052629
v  Velocity[y]            -8.2567          6.5859        -0.01011     -0.00040054
v  Velocity[z]            -10.427         0.88654         -3.1601         -5.3408
v  TurbEner            0.00058256          6.0405        0.064072         0.10003
v  Dissip              7.4261e-12          3.4139        0.017201        0.026663
v  TurbVisc                1.0188      1.2494e+06          1130.3          819.22
v  CourantNb                    0          2.8716         0.27964         0.45006
v  FourierNb           0.00016034          164.81         0.34671         0.22642
v  total_pressure           18022      1.4256e+05           95650           92416


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022877          164.81         0.62635         0.67648


 TIME FOR THE TIME STEP                8:        0.20680E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.970358067E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.80602E+01
   Friction velocity        uet   :  0.00000E+00 0.32972E+00
   Friction velocity        uk    :  0.13220E-01 0.69159E+00
   Dimensionless distance   yplus :  0.14402E+04 0.19590E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.32147E+05     311   0.29213E-02   0.11451E+00 
c  VelocityX    0.68931E+08      22   0.15820E-01   0.18909E-01 
c  VelocityY    0.68931E+08      22   0.15820E-01   0.16533E-01 
c  VelocityZ    0.68931E+08      22   0.15820E-01   0.37969E-01 
c  TurbEner     0.30066E+07     157   0.71518E-03   0.10793E-01 
c  Dissip       0.94238E+06     657   0.84339E-03   0.25810E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0027076                           327


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -83854           42012         -5691.4         -8931.8
v  Velocity[x]            -6.5954          6.3911      -0.0034784      -0.0056748
v  Velocity[y]            -8.3925          6.7095        -0.01039     -0.00061974
v  Velocity[z]            -10.606           1.044         -3.1602          -5.342
v  TurbEner            0.00058035          6.7243        0.068351         0.10619
v  Dissip              1.6669e-12          4.1683         0.01919        0.029237
v  TurbVisc               0.97029      4.5155e+06          1526.3          1062.8
v  CourantNb                    0          2.8716         0.27954         0.45002
v  FourierNb            0.0001917          633.98         0.44476         0.29276
v  total_pressure           17471      1.4334e+05           95634           92393


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0022873          633.98          0.7243         0.74278


 TIME FOR THE TIME STEP                9:        0.25754E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.306791975E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.81617E+01
   Friction velocity        uet   :  0.00000E+00 0.33197E+00
   Friction velocity        uk    :  0.13195E-01 0.66948E+00
   Dimensionless distance   yplus :  0.14380E+04 0.20820E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.30729E+05     310   0.27410E-02   0.10782E+00 
c  VelocityX    0.69001E+08      39   0.16658E-01   0.19225E-01 
c  VelocityY    0.69001E+08      39   0.16658E-01   0.14503E-01 
c  VelocityZ    0.69001E+08      39   0.16658E-01   0.35598E-01 
c  TurbEner     0.31641E+07    2684   0.66127E-02   0.93863E-02 
c  Dissip       0.10269E+07    5250   0.64002E-03   0.22331E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0017688                           343


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -85183           42978         -5561.8         -8714.1
v  Velocity[x]            -6.6475          6.4676      -0.0039248      -0.0061091
v  Velocity[y]            -8.4315          6.7491       -0.010477     -0.00066707
v  Velocity[z]            -10.724          1.2462         -3.1602          -5.343
v  TurbEner            0.00057815          7.1892        0.072552         0.11234
v  Dissip               7.551e-12          4.7387        0.021164        0.031842
v  TurbVisc                1.0022      2.0116e+07          3656.6          2017.1
v  CourantNb                    0          2.8714         0.27951         0.45002
v  FourierNb           0.00020981          4518.5          1.5542         0.70789
v  total_pressure           16142       1.443e+05           95763           92611


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017177          4518.5          1.8337          1.1579


 TIME FOR THE TIME STEP               10:        0.76457E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.322117854E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.84841E+01
   Friction velocity        uet   :  0.00000E+00 0.33546E+00
   Friction velocity        uk    :  0.13170E-01 0.63763E+00
   Dimensionless distance   yplus :  0.14359E+04 0.21543E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.31505E+05     315   0.26137E-02   0.11007E+00 
c  VelocityX    0.69065E+08      45   0.14979E-01   0.17274E-01 
c  VelocityY    0.69065E+08      45   0.14979E-01   0.15338E-01 
c  VelocityZ    0.69065E+08      45   0.14979E-01   0.32754E-01 
c  TurbEner     0.33096E+07    1388   0.22044E-02   0.76277E-02 
c  Dissip       0.11107E+07    1846   0.57782E-03   0.19069E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0039738                           303


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -85907           42243         -5443.7         -8527.6
v  Velocity[x]            -6.6632          6.4961      -0.0044233      -0.0067629
v  Velocity[y]            -8.4621          6.7361       -0.010621     -0.00076014
v  Velocity[z]            -10.756          1.4024         -3.1598          -5.343
v  TurbEner            0.00057596          7.4496        0.076413         0.11806
v  Dissip              9.3805e-12          5.1018        0.023066        0.034418
v  TurbVisc                1.1857      4.4401e+06          1981.7          1313.6
v  CourantNb                    0          2.8696         0.27956         0.45009
v  FourierNb           0.00023684          928.41         0.69569         0.40549
v  total_pressure           15418      1.4357e+05           95881           92797


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017187          928.41         0.97525         0.85558


 TIME FOR THE TIME STEP               11:        0.42164E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.285568828E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.86909E+01
   Friction velocity        uet   :  0.00000E+00 0.33619E+00
   Friction velocity        uk    :  0.13145E-01 0.63287E+00
   Dimensionless distance   yplus :  0.14338E+04 0.21826E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26078E+05     331   0.21236E-02   0.89962E-01 
c  VelocityX    0.69135E+08      33   0.14186E-01   0.10868E-01 
c  VelocityY    0.69135E+08      33   0.14186E-01   0.10633E-01 
c  VelocityZ    0.69135E+08      33   0.14186E-01   0.28800E-01 
c  TurbEner     0.34415E+07     874   0.16770E-02   0.64198E-02 
c  Dissip       0.11901E+07    1011   0.43511E-03   0.16403E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0013055                           303


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -84678           43972         -5240.5         -8187.5
v  Velocity[x]            -6.6494          6.5479      -0.0049709      -0.0074405
v  Velocity[y]            -8.4412          6.7813       -0.010734     -0.00073741
v  Velocity[z]            -10.791          1.5233         -3.1596         -5.3434
v  TurbEner            0.00057379          7.5262          0.0799         0.12326
v  Dissip              4.3336e-11          5.2607        0.024871        0.036927
v  TurbVisc                1.2944      3.5727e+06          2127.1          1630.1
v  CourantNb                    0          2.8677         0.27966          0.4502
v  FourierNb           0.00029488           875.7         0.75459         0.44888
v  total_pressure           16647       1.453e+05           96085           93138


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017202           875.7          1.0342         0.89908


 TIME FOR THE TIME STEP               12:        0.33983E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.192290743E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88609E+01
   Friction velocity        uet   :  0.00000E+00 0.33697E+00
   Friction velocity        uk    :  0.13120E-01 0.63038E+00
   Dimensionless distance   yplus :  0.14317E+04 0.21740E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26028E+05     307   0.20657E-02   0.88885E-01 
c  VelocityX    0.69217E+08      72   0.15588E-01   0.13060E-01 
c  VelocityY    0.69217E+08      72   0.15588E-01   0.10519E-01 
c  VelocityZ    0.69217E+08      72   0.15588E-01   0.28926E-01 
c  TurbEner     0.35692E+07      74   0.26717E-02   0.55182E-02 
c  Dissip       0.12645E+07      76   0.10184E-02   0.14880E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0022986                           294


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -87067           44008         -5231.5         -8184.8
v  Velocity[x]            -6.6844          7.0201      -0.0054526      -0.0080597
v  Velocity[y]            -8.5551          6.8756       -0.010466     -0.00039837
v  Velocity[z]            -10.775          1.6077         -3.1592         -5.3432
v  TurbEner            0.00057163          7.4378        0.083164          0.1282
v  Dissip              5.9792e-13          5.2288        0.026585        0.039378
v  TurbVisc                1.2899      7.7393e+05          1014.4          734.84
v  CourantNb                    0          2.8657         0.27977         0.45033
v  FourierNb           0.00032968          95.701         0.31661         0.20006
v  total_pressure           14258      1.4533e+05           96093           93140


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017226          95.701         0.59638         0.65038


 TIME FOR THE TIME STEP               13:        0.27268E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.367551949E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.89645E+01
   Friction velocity        uet   :  0.00000E+00 0.33644E+00
   Friction velocity        uk    :  0.13095E-01 0.61830E+00
   Dimensionless distance   yplus :  0.14296E+04 0.21410E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26572E+05     331   0.21313E-02   0.90019E-01 
c  VelocityX    0.69275E+08      18   0.15572E-01   0.10716E-01 
c  VelocityY    0.69275E+08      18   0.15572E-01   0.87249E-02 
c  VelocityZ    0.69275E+08      18   0.15572E-01   0.29203E-01 
c  TurbEner     0.36876E+07   10000   0.33340E-03   0.49049E-02 
c  Dissip       0.13343E+07   10000   0.34936E-03   0.14341E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00099479                           256


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -87401           44575         -5010.8         -7825.4
v  Velocity[x]            -6.6875          6.9365      -0.0061231      -0.0088155
v  Velocity[y]            -8.5501          6.9072       -0.010272     -3.9561e-05
v  Velocity[z]            -10.771          1.5986         -3.1588          -5.343
v  TurbEner            0.00056948          7.2278        0.086198         0.13283
v  Dissip              6.5022e-11          5.0546         0.02821        0.041762
v  TurbVisc                1.2856      5.6081e+07          8887.8          6454.4
v  CourantNb                    0          2.8631          0.2799         0.45049
v  FourierNb           0.00031426          9850.8          3.2469          2.1342
v  total_pressure           13924       1.459e+05           96314           93500


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017247          9850.8          3.5268          2.5847


 TIME FOR THE TIME STEP               14:        0.15211E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.246431965E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.90497E+01
   Friction velocity        uet   :  0.00000E+00 0.33624E+00
   Friction velocity        uk    :  0.13071E-01 0.60051E+00
   Dimensionless distance   yplus :  0.14276E+04 0.21550E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27164E+05     315   0.21011E-02   0.91756E-01 
c  VelocityX    0.69332E+08      43   0.15325E-01   0.13480E-01 
c  VelocityY    0.69332E+08      43   0.15325E-01   0.90121E-02 
c  VelocityZ    0.69332E+08      43   0.15325E-01   0.26261E-01 
c  TurbEner     0.37986E+07      46   0.33788E-03   0.43746E-02 
c  Dissip       0.14005E+07      55   0.36684E-03   0.13690E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0013278                           290


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -86774           45382         -4880.6         -7614.6
v  Velocity[x]            -6.7397           7.657      -0.0067429       -0.009778
v  Velocity[y]            -8.5292          6.8397      -0.0099796      0.00043522
v  Velocity[z]            -10.732           1.644         -3.1584         -5.3427
v  TurbEner            0.00056732          6.9417        0.089039         0.13722
v  Dissip              9.7325e-11          4.7917        0.029737        0.044053
v  TurbVisc                1.2814      5.1577e+05          1161.8          849.45
v  CourantNb                    0           2.861         0.28006         0.45069
v  FourierNb           0.00044492          107.62         0.38681         0.24263
v  total_pressure           14551      1.4671e+05           96444           93710


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017267          107.62         0.66687         0.69332


 TIME FOR THE TIME STEP               15:        0.20695E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.271075471E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.90805E+01
   Friction velocity        uet   :  0.00000E+00 0.33489E+00
   Friction velocity        uk    :  0.13046E-01 0.59201E+00
   Dimensionless distance   yplus :  0.14255E+04 0.21451E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24124E+05     329   0.16975E-02   0.81461E-01 
c  VelocityX    0.69401E+08      18   0.12510E-01   0.94133E-02 
c  VelocityY    0.69401E+08      18   0.12510E-01   0.72112E-02 
c  VelocityZ    0.69401E+08      18   0.12510E-01   0.25690E-01 
c  TurbEner     0.39031E+07      22   0.33179E-03   0.39551E-02 
c  Dissip       0.14635E+07      48   0.32289E-03   0.12818E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00091823                           263


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -86333           47185         -4629.5         -7204.8
v  Velocity[x]            -6.6944          7.3857      -0.0075235       -0.010649
v  Velocity[y]            -8.6361          6.8201      -0.0095437        0.001203
v  Velocity[z]            -10.734          1.6706         -3.1582         -5.3429
v  TurbEner            0.00056514          6.6337        0.091724          0.1414
v  Dissip              6.4217e-12          4.5015        0.031185        0.046259
v  TurbVisc                1.2774      3.4445e+05          955.14          721.05
v  CourantNb                    0          2.8593         0.28022         0.45092
v  FourierNb           0.00040672          53.599         0.30203         0.19725
v  total_pressure           14992      1.4851e+05           96696           94120


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017283          53.599         0.58225         0.64817


 TIME FOR THE TIME STEP               16:        0.20435E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.395200136E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.91268E+01
   Friction velocity        uet   :  0.00000E+00 0.33485E+00
   Friction velocity        uk    :  0.13021E-01 0.58321E+00
   Dimensionless distance   yplus :  0.14235E+04 0.21133E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23095E+05     295   0.15662E-02   0.77325E-01 
c  VelocityX    0.69488E+08      17   0.14032E-01   0.79615E-02 
c  VelocityY    0.69488E+08      17   0.14032E-01   0.64110E-02 
c  VelocityZ    0.69488E+08      17   0.14032E-01   0.24481E-01 
c  TurbEner     0.40036E+07    2031   0.33602E-03   0.37719E-02 
c  Dissip       0.15244E+07    1891   0.32541E-03   0.12018E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0078498                           262


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -86933           47040         -4589.1         -7152.1
v  Velocity[x]            -6.7236          7.1346      -0.0083792       -0.011842
v  Velocity[y]            -8.6654          6.8178      -0.0089964       0.0020738
v  Velocity[z]            -10.697          1.6817         -3.1576         -5.3425
v  TurbEner            0.00056297          6.3147        0.094343         0.14552
v  Dissip              3.3035e-11          4.1979        0.032563         0.04839
v  TurbVisc                1.2735      5.2159e+06          1684.5          1331.6
v  CourantNb                    0          2.8604         0.28036         0.45116
v  FourierNb           0.00040503          797.33         0.54342         0.38973
v  total_pressure           14392      1.4836e+05           96736           94173


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017306          797.33         0.82378         0.84089


 TIME FOR THE TIME STEP               17:        0.44766E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.907263444E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.91266E+01
   Friction velocity        uet   :  0.00000E+00 0.33373E+00
   Friction velocity        uk    :  0.12996E-01 0.56954E+00
   Dimensionless distance   yplus :  0.14215E+04 0.20637E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22465E+05     327   0.16368E-02   0.74635E-01 
c  VelocityX    0.69545E+08      19   0.16084E-01   0.80566E-02 
c  VelocityY    0.69545E+08      19   0.16084E-01   0.77907E-02 
c  VelocityZ    0.69545E+08      19   0.16084E-01   0.22935E-01 
c  TurbEner     0.41029E+07     105   0.88339E-03   0.36427E-02 
c  Dissip       0.15824E+07     179   0.28592E-03   0.10949E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00065347                           277


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -85647           48213         -4237.6         -6578.1
v  Velocity[x]            -6.7454          6.9203      -0.0089783       -0.012603
v  Velocity[y]            -8.5895          6.8597      -0.0083867       0.0030535
v  Velocity[z]            -10.689          1.6801         -3.1573         -5.3423
v  TurbEner            0.00056082          6.2992        0.096897         0.14961
v  Dissip              5.3411e-11           4.376        0.033872        0.050452
v  TurbVisc                1.2697      1.0152e+06          1090.1          859.58
v  CourantNb                    0          2.8621         0.28053         0.45144
v  FourierNb            0.0004331          129.53          0.3468         0.23501
v  total_pressure           15678      1.4954e+05           97087           94747


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017317          129.53         0.62733         0.68645


 TIME FOR THE TIME STEP               18:        0.22272E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.255517299E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.91247E+01
   Friction velocity        uet   :  0.00000E+00 0.33310E+00
   Friction velocity        uk    :  0.12971E-01 0.55267E+00
   Dimensionless distance   yplus :  0.14195E+04 0.20026E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25156E+05     326   0.17388E-02   0.83515E-01 
c  VelocityX    0.69611E+08      18   0.13966E-01   0.10374E-01 
c  VelocityY    0.69611E+08      18   0.13966E-01   0.73157E-02 
c  VelocityZ    0.69611E+08      18   0.13966E-01   0.21809E-01 
c  TurbEner     0.41937E+07      34   0.32058E-03   0.31207E-02 
c  Dissip       0.16378E+07     122   0.28783E-03   0.98388E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0016416                           250


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -87172           49132         -4029.8         -6234.7
v  Velocity[x]            -6.6553           6.764      -0.0097307       -0.013789
v  Velocity[y]            -8.6394          6.8845      -0.0078915        0.003717
v  Velocity[z]            -10.657          1.7622         -3.1567         -5.3419
v  TurbEner            0.00055868          6.5243        0.099254          0.1534
v  Dissip              1.7711e-11          4.6239        0.035109        0.052435
v  TurbVisc                 1.266       6.278e+05          1282.5          859.41
v  CourantNb                    0           2.863         0.28068         0.45171
v  FourierNb           0.00053484          86.268         0.39507         0.24197
v  total_pressure           14153      1.5046e+05           97295           95090


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017323          86.268         0.67576         0.69369


 TIME FOR THE TIME STEP               19:        0.21458E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.155027576E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.91027E+01
   Friction velocity        uet   :  0.00000E+00 0.33224E+00
   Friction velocity        uk    :  0.12946E-01 0.53381E+00
   Dimensionless distance   yplus :  0.14175E+04 0.19343E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22509E+05     303   0.15375E-02   0.74628E-01 
c  VelocityX    0.69678E+08      56   0.14745E-01   0.87474E-02 
c  VelocityY    0.69678E+08      56   0.14745E-01   0.69646E-02 
c  VelocityZ    0.69678E+08      56   0.14745E-01   0.18804E-01 
c  TurbEner     0.42955E+07     201   0.79048E-02   0.34944E-02 
c  Dissip       0.16904E+07     458   0.82619E-03   0.87562E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0096143                           225


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -85792           49883         -3654.2         -5622.5
v  Velocity[x]            -6.7176          6.6315        -0.01038       -0.014693
v  Velocity[y]            -8.6477          6.8303      -0.0077219       0.0039829
v  Velocity[z]            -10.658          1.8452         -3.1564         -5.3416
v  TurbEner            0.00055656          6.7242         0.10176         0.15749
v  Dissip              9.7619e-12           4.841        0.036271         0.05433
v  TurbVisc                1.2625      1.8925e+06          1360.2          1062.9
v  CourantNb                    0           2.862         0.28084         0.45199
v  FourierNb           0.00057401          220.56         0.42992          0.2873
v  total_pressure           15533      1.5121e+05           97671           95703


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017318          220.56         0.71075         0.73929


 TIME FOR THE TIME STEP               20:        0.24710E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.345470913E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.90942E+01
   Friction velocity        uet   :  0.00000E+00 0.33231E+00
   Friction velocity        uk    :  0.12922E-01 0.51394E+00
   Dimensionless distance   yplus :  0.14155E+04 0.18623E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24410E+05     315   0.16434E-02   0.80930E-01 
c  VelocityX    0.69752E+08      47   0.16422E-01   0.96083E-02 
c  VelocityY    0.69752E+08      47   0.16422E-01   0.71733E-02 
c  VelocityZ    0.69752E+08      47   0.16422E-01   0.20716E-01 
c  TurbEner     0.43849E+07     138   0.40077E-02   0.36850E-02 
c  Dissip       0.17392E+07     104   0.10160E-02   0.79634E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip         -0.037586                           226


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -84828           51604         -3237.2         -4930.6
v  Velocity[x]            -6.7155          6.5468       -0.010907       -0.015499
v  Velocity[y]            -8.7748           6.813      -0.0073744        0.004482
v  Velocity[z]            -10.691           1.912         -3.1559         -5.3415
v  TurbEner            0.00055445           6.862         0.10421         0.16158
v  Dissip              5.3174e-12          4.9895        0.037381         0.05618
v  TurbVisc                 1.259      3.4363e+06          1416.2          943.55
v  CourantNb                    0           2.862         0.28099         0.45229
v  FourierNb           0.00059264          389.75         0.40565         0.25123
v  total_pressure           16497      1.5293e+05           98088           96394


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017313          389.75         0.68665         0.70352


 TIME FOR THE TIME STEP               21:        0.22573E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.118019037E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.90547E+01
   Friction velocity        uet   :  0.00000E+00 0.33166E+00
   Friction velocity        uk    :  0.12897E-01 0.49379E+00
   Dimensionless distance   yplus :  0.14135E+04 0.17892E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28368E+05     304   0.18965E-02   0.93842E-01 
c  VelocityX    0.69812E+08      18   0.15350E-01   0.76046E-02 
c  VelocityY    0.69812E+08      18   0.15350E-01   0.93330E-02 
c  VelocityZ    0.69812E+08      18   0.15350E-01   0.21334E-01 
c  TurbEner     0.44689E+07     640   0.50756E-03   0.28845E-02 
c  Dissip       0.17837E+07     780   0.23772E-03   0.74332E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00072889                           215


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -84428           52880           -2810         -4227.9
v  Velocity[x]            -6.7373          6.5551       -0.011543       -0.016384
v  Velocity[y]            -8.7721          6.9064      -0.0071959       0.0045947
v  Velocity[z]            -10.648          1.9925         -3.1556         -5.3413
v  TurbEner            0.00055236          6.9805         0.10639         0.16528
v  Dissip              5.0873e-12          5.1135        0.038424        0.057955
v  TurbVisc                1.2556      6.3059e+06            1752          1022.5
v  CourantNb                    0          2.8599         0.28114         0.45258
v  FourierNb            0.0006117          988.86          0.5503         0.29721
v  total_pressure           16897      1.5421e+05           98515           97097


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017311          988.86         0.83144         0.74979


 TIME FOR THE TIME STEP               22:        0.30155E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.156370232E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393705E+07
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 0.90437E+01
   Friction velocity        uet   :  0.00000E+00 0.33240E+00
   Friction velocity        uk    :  0.12873E-01 0.47394E+00
   Dimensionless distance   yplus :  0.14116E+04 0.17173E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25967E+05     309   0.15686E-02   0.85885E-01 
c  VelocityX    0.69886E+08      17   0.13863E-01   0.83342E-02 
c  VelocityY    0.69886E+08      17   0.13863E-01   0.56940E-02 
c  VelocityZ    0.69886E+08      17   0.13863E-01   0.18451E-01 
c  TurbEner     0.45548E+07     136   0.23186E-03   0.25598E-02 
c  Dissip       0.18249E+07     177   0.23280E-03   0.69073E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00063541                           228


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -82269           53388           -2391         -3544.1
v  Velocity[x]            -6.7433          6.5448       -0.011906       -0.016929
v  Velocity[y]            -8.7009          6.8691      -0.0073908       0.0041785
v  Velocity[z]            -10.676          2.1103         -3.1551         -5.3405
v  TurbEner            0.00055029          7.0392         0.10838         0.16871
v  Dissip              4.3272e-11          5.1682         0.03935        0.059601
v  TurbVisc                1.2523      6.5909e+06          2072.2          1527.8
v  CourantNb                    0           2.859         0.28131         0.45293
v  FourierNb           0.00066016          744.31         0.59956         0.39552
v  total_pressure           19056      1.5471e+05           98934           97781


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017317          744.31         0.88086         0.84845


 TIME FOR THE TIME STEP               23:        0.22858E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.158418123E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.89904E+01
   Friction velocity        uet   :  0.00000E+00 0.33192E+00
   Friction velocity        uk    :  0.12849E-01 0.45482E+00
   Dimensionless distance   yplus :  0.14097E+04 0.17002E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27540E+05     329   0.18221E-02   0.91043E-01 
c  VelocityX    0.69923E+08      17   0.15042E-01   0.66213E-02 
c  VelocityY    0.69923E+08      17   0.15042E-01   0.62605E-02 
c  VelocityZ    0.69923E+08      17   0.15042E-01   0.18710E-01 
c  TurbEner     0.46411E+07      28   0.21509E-03   0.24334E-02 
c  Dissip       0.18638E+07     132   0.23780E-03   0.65941E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip         -0.015266                           218


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -80320           55320           -1801         -2558.9
v  Velocity[x]            -6.7971          6.5147       -0.012303       -0.017489
v  Velocity[y]            -8.6606           6.845      -0.0074874       0.0039574
v  Velocity[z]            -10.724          2.1586         -3.1544         -5.3395
v  TurbEner            0.00054824          7.0393          0.1103         0.17208
v  Dissip              4.1481e-11          5.1578        0.040222        0.061188
v  TurbVisc                 1.249      7.7508e+05          1122.4          872.39
v  CourantNb                    0          2.8554         0.28146         0.45325
v  FourierNb            0.0007377          76.583         0.33294          0.2249
v  total_pressure           21005      1.5664e+05           99524           98766


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017313          76.583          0.6144         0.67815


 TIME FOR THE TIME STEP               24:        0.22196E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.319471502E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.89552E+01
   Friction velocity        uet   :  0.00000E+00 0.33242E+00
   Friction velocity        uk    :  0.12825E-01 0.43667E+00
   Dimensionless distance   yplus :  0.14077E+04 0.17247E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12


 Write intermediate restart files
   checkpoint at iteration         25, Physical time    0.25000E+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:    0.38478E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.32003E+05     344   0.24353E-02   0.10560E+00 
c  VelocityX    0.69965E+08      17   0.16251E-01   0.66671E-02 
c  VelocityY    0.69965E+08      17   0.16251E-01   0.64725E-02 
c  VelocityZ    0.69965E+08      17   0.16251E-01   0.16171E-01 
c  TurbEner     0.47277E+07      36   0.21074E-03   0.23793E-02 
c  Dissip       0.19008E+07      60   0.22400E-03   0.64772E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00053642                           214


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -78234           58126         -579.36         -517.24
v  Velocity[x]            -6.8235          6.5211       -0.012753       -0.018256
v  Velocity[y]            -8.7388          6.8629      -0.0078165       0.0033986
v  Velocity[z]             -10.74          2.1974         -3.1537         -5.3386
v  TurbEner             0.0005462          7.0038         0.11215         0.17535
v  Dissip              1.2204e-11          5.1099        0.041024        0.062684
v  TurbVisc                1.2458      8.0813e+05          1000.4          719.23
v  CourantNb                    0           2.854         0.28161         0.45354
v  FourierNb           0.00081058          148.98          0.3177         0.20505
v  total_pressure           23091      1.5945e+05      1.0075e+05      1.0081e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0017282          148.98         0.59931          0.6586


 TIME FOR THE TIME STEP               25:        0.30390E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.105255715E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.88991E+01
   Friction velocity        uet   :  0.00000E+00 0.33244E+00
   Friction velocity        uk    :  0.12801E-01 0.42825E+00
   Dimensionless distance   yplus :  0.14058E+04 0.17452E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.33021E+05     343   0.25187E-02   0.10868E+00 
c  VelocityX    0.70016E+08      18   0.14946E-01   0.10397E-01 
c  VelocityY    0.70016E+08      18   0.14946E-01   0.60004E-02 
c  VelocityZ    0.70016E+08      18   0.14946E-01   0.15796E-01 
c  TurbEner     0.48159E+07     242   0.21493E-03   0.23548E-02 
c  Dissip       0.19385E+07     276   0.22801E-03   0.64791E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -8.7509e-05                           207


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -75395           61434          478.64          1260.7
v  Velocity[x]            -6.8907          6.4873       -0.013053       -0.018948
v  Velocity[y]            -8.7426          6.8749      -0.0081221       0.0029079
v  Velocity[z]            -10.665          2.2694          -3.153         -5.3378
v  TurbEner            0.00054418          6.9767         0.11391         0.17853
v  Dissip              2.8648e-11           5.073         0.04178        0.064133
v  TurbVisc                1.2426      2.7488e+06          1470.7          1011.8
v  CourantNb                    0          2.8509         0.28172          0.4538
v  FourierNb            0.0008122          366.03         0.43464         0.27202
v  total_pressure           25930      1.6276e+05       1.018e+05      1.0259e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0016853          366.03         0.71637         0.72582


 TIME FOR THE TIME STEP               26:        0.25005E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.127220260E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.88604E+01
   Friction velocity        uet   :  0.00000E+00 0.33338E+00
   Friction velocity        uk    :  0.12777E-01 0.42576E+00
   Dimensionless distance   yplus :  0.14039E+04 0.17627E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.29841E+05     351   0.22756E-02   0.97464E-01 
c  VelocityX    0.70062E+08      27   0.17005E-01   0.74592E-02 
c  VelocityY    0.70062E+08      27   0.17005E-01   0.51092E-02 
c  VelocityZ    0.70062E+08      27   0.17005E-01   0.13864E-01 
c  TurbEner     0.49085E+07      94   0.17048E-02   0.24686E-02 
c  Dissip       0.19765E+07     177   0.23693E-03   0.67630E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0010936                           215


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -71934           64068          1615.9          3156.8
v  Velocity[x]            -6.8907          6.4954        -0.01327       -0.019385
v  Velocity[y]             -8.734          6.8524      -0.0084398       0.0023305
v  Velocity[z]            -10.652           2.335         -3.1524         -5.3369
v  TurbEner            0.00054217          6.9191         0.11569         0.18179
v  Dissip              3.6795e-11          5.0293        0.042487        0.065535
v  TurbVisc                1.2394      1.1698e+06          1293.3          956.35
v  CourantNb                    0          2.8485         0.28184         0.45404
v  FourierNb           0.00082045          177.56         0.40419         0.26222
v  total_pressure           29391      1.6539e+05      1.0294e+05      1.0448e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0016105          177.56         0.68603         0.71626


 TIME FOR THE TIME STEP               27:        0.22412E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.158630283E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.87797E+01
   Friction velocity        uet   :  0.00000E+00 0.33296E+00
   Friction velocity        uk    :  0.12753E-01 0.42254E+00
   Dimensionless distance   yplus :  0.14020E+04 0.17802E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28390E+05     326   0.20274E-02   0.92446E-01 
c  VelocityX    0.70102E+08      18   0.14385E-01   0.94779E-02 
c  VelocityY    0.70102E+08      18   0.14385E-01   0.60526E-02 
c  VelocityZ    0.70102E+08      18   0.14385E-01   0.13284E-01 
c  TurbEner     0.50011E+07      27   0.34119E-03   0.25150E-02 
c  Dissip       0.20156E+07      19   0.25010E-03   0.73942E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.7239e-07                           185


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69923           66531          2503.6          4645.9
v  Velocity[x]            -6.8454          6.4775       -0.013447         -0.0197
v  Velocity[y]            -8.7587          6.8513      -0.0087197       0.0017542
v  Velocity[z]            -10.659          2.3996          -3.152         -5.3366
v  TurbEner            0.00054017          6.8394         0.11731         0.18486
v  Dissip              6.4124e-12          5.1059        0.043147        0.066892
v  TurbVisc                1.2364      9.1066e+05          936.55          701.55
v  CourantNb                    0          2.8439         0.28193         0.45423
v  FourierNb           0.00080768          116.22         0.28858         0.18972
v  total_pressure           31402      1.6786e+05      1.0383e+05      1.0597e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001448          116.22         0.57052         0.64396


 TIME FOR THE TIME STEP               28:        0.20830E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.211692963E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.87391E+01
   Friction velocity        uet   :  0.00000E+00 0.33431E+00
   Friction velocity        uk    :  0.12730E-01 0.41822E+00
   Dimensionless distance   yplus :  0.14002E+04 0.17985E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23514E+05     326   0.16753E-02   0.76221E-01 
c  VelocityX    0.70153E+08      18   0.14429E-01   0.73992E-02 
c  VelocityY    0.70153E+08      18   0.14429E-01   0.41751E-02 
c  VelocityZ    0.70153E+08      18   0.14429E-01   0.11996E-01 
c  TurbEner     0.50968E+07     444   0.17301E-03   0.22502E-02 
c  Dissip       0.20556E+07     268   0.17647E-03   0.62784E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00067618                           202


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -71922           67535          2952.1          5396.6
v  Velocity[x]            -6.8552          6.5017       -0.013797       -0.020234
v  Velocity[y]            -8.8926          6.8782      -0.0092998       0.0006539
v  Velocity[z]             -10.77          2.4528         -3.1516         -5.3362
v  TurbEner            0.00053819          6.7864         0.11889         0.18788
v  Dissip              2.5619e-11          5.1686        0.043768        0.068195
v  TurbVisc                1.2333      5.2294e+06          1501.8          1077.2
v  CourantNb                    0          2.8422           0.282          0.4544
v  FourierNb           0.00082345          601.57         0.41114         0.27496
v  total_pressure           29403      1.6886e+05      1.0428e+05      1.0672e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014439          601.57         0.69315         0.72936


 TIME FOR THE TIME STEP               29:        0.25243E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.107458375E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.87359E+01
   Friction velocity        uet   :  0.00000E+00 0.33494E+00
   Friction velocity        uk    :  0.12707E-01 0.41641E+00
   Dimensionless distance   yplus :  0.13983E+04 0.18184E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22673E+05     309   0.15679E-02   0.73459E-01 
c  VelocityX    0.70201E+08      17   0.15420E-01   0.60155E-02 
c  VelocityY    0.70201E+08      17   0.15420E-01   0.48023E-02 
c  VelocityZ    0.70201E+08      17   0.15420E-01   0.12473E-01 
c  TurbEner     0.51943E+07      37   0.21041E-03   0.22654E-02 
c  Dissip       0.20959E+07      26   0.16315E-03   0.63593E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -7.7871e-07                           212


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -70059           68732            3306          5981.5
v  Velocity[x]            -6.8667          6.4664       -0.013934       -0.020605
v  Velocity[y]            -8.9285          6.9132      -0.0096786     -6.1277e-05
v  Velocity[z]            -10.771          2.5058         -3.1513          -5.336
v  TurbEner            0.00053622          6.6994         0.12039         0.19081
v  Dissip              1.6628e-11          5.2127        0.044347        0.069446
v  TurbVisc                1.2304      1.3084e+06          1472.8          1017.9
v  CourantNb                    0          2.8376         0.28207         0.45457
v  FourierNb           0.00075772          178.48         0.43756         0.27744
v  total_pressure           31266      1.7006e+05      1.0463e+05      1.0731e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014399          178.48         0.71963         0.73201


 TIME FOR THE TIME STEP               30:        0.21142E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.294760743E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.87505E+01
   Friction velocity        uet   :  0.00000E+00 0.33605E+00
   Friction velocity        uk    :  0.12683E-01 0.41445E+00
   Dimensionless distance   yplus :  0.13965E+04 0.18405E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24199E+05     256   0.14213E-02   0.78199E-01 
c  VelocityX    0.70242E+08      27   0.17549E-01   0.55809E-02 
c  VelocityY    0.70242E+08      27   0.17549E-01   0.59565E-02 
c  VelocityZ    0.70242E+08      27   0.17549E-01   0.11782E-01 
c  TurbEner     0.52999E+07     134   0.10837E-02   0.24536E-02 
c  Dissip       0.21402E+07      93   0.16434E-03   0.70970E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0010196                           191


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68418           68518          3263.4          5902.4
v  Velocity[x]            -6.8915          6.4593       -0.014291       -0.021107
v  Velocity[y]            -8.8875          6.9157       -0.010302      -0.0011867
v  Velocity[z]            -10.743          2.5507         -3.1508         -5.3354
v  TurbEner            0.00053427          6.6021         0.12191         0.19382
v  Dissip              8.2072e-11          5.2441        0.044897        0.070687
v  TurbVisc                1.2275       2.016e+06          1323.8             895
v  CourantNb                    0          2.8347         0.28212         0.45469
v  FourierNb           0.00074064          293.48          0.3925         0.24144
v  total_pressure           32907      1.6984e+05      1.0459e+05      1.0723e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001436          293.48         0.67462         0.69613


 TIME FOR THE TIME STEP               31:        0.24484E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.345997402E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.87862E+01
   Friction velocity        uet   :  0.00000E+00 0.33614E+00
   Friction velocity        uk    :  0.12660E-01 0.41148E+00
   Dimensionless distance   yplus :  0.13946E+04 0.18638E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25332E+05     295   0.16090E-02   0.81700E-01 
c  VelocityX    0.70251E+08      18   0.15179E-01   0.95475E-02 
c  VelocityY    0.70251E+08      18   0.15179E-01   0.49108E-02 
c  VelocityZ    0.70251E+08      18   0.15179E-01   0.11569E-01 
c  TurbEner     0.54059E+07      19   0.26999E-03   0.23454E-02 
c  Dissip       0.21875E+07      54   0.16192E-03   0.68365E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.2099e-07                           197


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66868           69464            3306          5967.8
v  Velocity[x]            -6.8552          6.5143        -0.01436       -0.021506
v  Velocity[y]            -8.8524          7.0074       -0.010551       -0.001668
v  Velocity[z]            -10.769          2.6178         -3.1509         -5.3355
v  TurbEner            0.00053233          6.6636         0.12334         0.19668
v  Dissip              5.1394e-14          5.2542        0.045442        0.071913
v  TurbVisc                1.2246      4.0833e+05          1003.8          747.26
v  CourantNb                    0            2.83         0.28219         0.45483
v  FourierNb           0.00072736          56.746         0.29862         0.19897
v  total_pressure           34457      1.7079e+05      1.0463e+05      1.0729e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014321          56.746         0.58081          0.6538


 TIME FOR THE TIME STEP               32:        0.23366E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.971362970E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88222E+01
   Friction velocity        uet   :  0.00000E+00 0.33765E+00
   Friction velocity        uk    :  0.12637E-01 0.41803E+00
   Dimensionless distance   yplus :  0.13928E+04 0.18884E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25632E+05     279   0.15754E-02   0.82736E-01 
c  VelocityX    0.70302E+08      17   0.17459E-01   0.69576E-02 
c  VelocityY    0.70302E+08      17   0.17459E-01   0.45372E-02 
c  VelocityZ    0.70302E+08      17   0.17459E-01   0.11179E-01 
c  TurbEner     0.55160E+07   10000   0.15062E-03   0.22902E-02 
c  Dissip       0.22368E+07   10000   0.15500E-03   0.68369E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00030042                           203


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68406           68523          3153.2          5699.7
v  Velocity[x]            -6.8837          6.4443       -0.014435       -0.021817
v  Velocity[y]            -8.9645           7.026       -0.011237      -0.0028308
v  Velocity[z]            -10.843          2.6712         -3.1504          -5.335
v  TurbEner             0.0005304          6.7123         0.12473          0.1995
v  Dissip              4.1755e-12          5.2535        0.045963        0.073102
v  TurbVisc                1.2218      6.5204e+08           82197           65466
v  CourantNb                    0          2.8294         0.28221         0.45493
v  FourierNb           0.00077482      1.0968e+05            29.3           21.97
v  total_pressure           32919      1.6985e+05      1.0448e+05      1.0702e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014284      1.0968e+05          29.582          22.425


 TIME FOR THE TIME STEP               33:        0.15690E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.125162766E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88820E+01
   Friction velocity        uet   :  0.00000E+00 0.33788E+00
   Friction velocity        uk    :  0.12614E-01 0.42656E+00
   Dimensionless distance   yplus :  0.13910E+04 0.19131E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26698E+05     293   0.16636E-02   0.86108E-01 
c  VelocityX    0.70309E+08      17   0.16151E-01   0.83931E-02 
c  VelocityY    0.70309E+08      17   0.16151E-01   0.56305E-02 
c  VelocityZ    0.70309E+08      17   0.16151E-01   0.11346E-01 
c  TurbEner     0.56256E+07     611   0.13381E-03   0.21519E-02 
c  Dissip       0.22865E+07    1989   0.14718E-03   0.64029E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00029394                           182


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68678           68793          2956.8          5365.3
v  Velocity[x]            -6.9046          6.4622       -0.014404       -0.021899
v  Velocity[y]            -8.9621          7.0757       -0.011753      -0.0039159
v  Velocity[z]            -10.809           2.706         -3.1503         -5.3348
v  TurbEner            0.00052848          6.7435         0.12607         0.20223
v  Dissip              8.3687e-12          5.2336        0.046449         0.07424
v  TurbVisc                 1.219      8.0261e+06          2118.9            1885
v  CourantNb                    0          2.8215         0.28226         0.45503
v  FourierNb           0.00070876          974.95         0.62829         0.47855
v  total_pressure           32647      1.7012e+05      1.0428e+05      1.0669e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014254          974.95         0.91055         0.93358


 TIME FOR THE TIME STEP               34:        0.42375E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.223062789E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.89435E+01
   Friction velocity        uet   :  0.00000E+00 0.33952E+00
   Friction velocity        uk    :  0.12591E-01 0.43483E+00
   Dimensionless distance   yplus :  0.13892E+04 0.19368E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27729E+05     294   0.18513E-02   0.89449E-01 
c  VelocityX    0.70346E+08      17   0.15355E-01   0.58336E-02 
c  VelocityY    0.70346E+08      17   0.15355E-01   0.47212E-02 
c  VelocityZ    0.70346E+08      17   0.15355E-01   0.11005E-01 
c  TurbEner     0.57361E+07     358   0.12613E-03   0.20680E-02 
c  Dissip       0.23380E+07     389   0.14011E-03   0.60768E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00019569                           204


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68671           67891          2835.5          5151.7
v  Velocity[x]            -6.8161          6.4768       -0.014407       -0.021959
v  Velocity[y]            -8.9113          7.0899       -0.012545      -0.0053723
v  Velocity[z]            -10.811          2.6222         -3.1499         -5.3343
v  TurbEner            0.00052658          6.7682         0.12737         0.20489
v  Dissip              5.4486e-12          5.2063        0.046917        0.075342
v  TurbVisc                1.2162      4.0034e+06          1589.8            1096
v  CourantNb                    0          2.8237         0.28229         0.45511
v  FourierNb           0.00070223          735.55          0.4901         0.31882
v  total_pressure           32654      1.6922e+05      1.0416e+05      1.0648e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014222          735.55         0.77239         0.77393


 TIME FOR THE TIME STEP               35:        0.32771E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.177872774E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.89597E+01
   Friction velocity        uet   :  0.00000E+00 0.34030E+00
   Friction velocity        uk    :  0.12569E-01 0.44274E+00
   Dimensionless distance   yplus :  0.13874E+04 0.19590E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25612E+05     279   0.16693E-02   0.82294E-01 
c  VelocityX    0.70362E+08      18   0.15779E-01   0.75469E-02 
c  VelocityY    0.70362E+08      18   0.15779E-01   0.40822E-02 
c  VelocityZ    0.70362E+08      18   0.15779E-01   0.93900E-02 
c  TurbEner     0.58477E+07     479   0.19634E-03   0.20334E-02 
c  Dissip       0.23902E+07     847   0.13530E-03   0.61246E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0003219                           201


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69279           68453            2764          5027.2
v  Velocity[x]            -6.8822          6.5033       -0.013976       -0.021224
v  Velocity[y]            -8.9168          7.1485       -0.013188      -0.0067096
v  Velocity[z]             -10.83          2.6059         -3.1499         -5.3344
v  TurbEner            0.00052469          6.7765         0.12864         0.20752
v  Dissip               1.564e-11          5.1619         0.04737        0.076415
v  TurbVisc                1.2135      6.1523e+06          2224.6          1307.7
v  CourantNb                    0          2.8173         0.28231         0.45518
v  FourierNb           0.00073087          1372.6         0.71879         0.40309
v  total_pressure           32046      1.6978e+05      1.0409e+05      1.0635e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014191          1372.6          1.0011         0.85828


 TIME FOR THE TIME STEP               36:        0.44698E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.173099506E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.89875E+01
   Friction velocity        uet   :  0.00000E+00 0.34168E+00
   Friction velocity        uk    :  0.12546E-01 0.45046E+00
   Dimensionless distance   yplus :  0.13857E+04 0.19793E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27445E+05     288   0.17423E-02   0.88205E-01 
c  VelocityX    0.70383E+08      17   0.17274E-01   0.51636E-02 
c  VelocityY    0.70383E+08      17   0.17274E-01   0.47502E-02 
c  VelocityZ    0.70383E+08      17   0.17274E-01   0.14581E-01 
c  TurbEner     0.59623E+07      98   0.13407E-03   0.20634E-02 
c  Dissip       0.24461E+07      98   0.13377E-03   0.63583E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -3.1266e-05                           197


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -70602           67531          2774.4          5030.1
v  Velocity[x]            -6.8468          6.5224       -0.013573        -0.02049
v  Velocity[y]            -9.0048          7.1463        -0.01405      -0.0083657
v  Velocity[z]            -10.901          2.5866         -3.1494         -5.3337
v  TurbEner            0.00052282          6.8119         0.12989          0.2101
v  Dissip              2.1187e-11          5.1544        0.047818        0.077479
v  TurbVisc                1.2109      2.1434e+06          1533.9          1092.3
v  CourantNb                    0          2.8182         0.28232         0.45523
v  FourierNb           0.00069334          195.01         0.43405         0.28155
v  total_pressure           30723      1.6886e+05       1.041e+05      1.0636e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001416          195.01         0.71637         0.73678


 TIME FOR THE TIME STEP               37:        0.29219E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.856757312E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.89902E+01
   Friction velocity        uet   :  0.00000E+00 0.34161E+00
   Friction velocity        uk    :  0.12524E-01 0.45769E+00
   Dimensionless distance   yplus :  0.13839E+04 0.19978E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26548E+05     296   0.17870E-02   0.85269E-01 
c  VelocityX    0.70386E+08      78   0.16849E-01   0.70885E-02 
c  VelocityY    0.70386E+08      78   0.16849E-01   0.71548E-02 
c  VelocityZ    0.70386E+08      78   0.16849E-01   0.12701E-01 
c  TurbEner     0.60960E+07      98   0.92317E-02   0.32769E-02 
c  Dissip       0.25099E+07     199   0.22231E-03   0.84024E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -0.00060522                           176


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -70307           69205          2998.1          5406.4
v  Velocity[x]            -6.8432          6.5018       -0.012924         -0.0196
v  Velocity[y]            -8.9616          7.1576       -0.014975       -0.010364
v  Velocity[z]            -10.877          2.5584         -3.1494         -5.3336
v  TurbEner            0.00052096          6.8341         0.13139         0.21312
v  Dissip              6.1484e-12           5.132        0.048298        0.078601
v  TurbVisc                1.2083       1.582e+06            1336          933.07
v  CourantNb                    0          2.8129         0.28233         0.45528
v  FourierNb           0.00070671          287.39         0.42608         0.26414
v  total_pressure           31018      1.7053e+05      1.0432e+05      1.0673e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001413          287.39         0.70841         0.71942


 TIME FOR THE TIME STEP               38:        0.29850E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.157408204E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.90163E+01
   Friction velocity        uet   :  0.00000E+00 0.34344E+00
   Friction velocity        uk    :  0.12501E-01 0.46469E+00
   Dimensionless distance   yplus :  0.13822E+04 0.20144E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25378E+05     291   0.16807E-02   0.81273E-01 
c  VelocityX    0.70420E+08      41   0.15707E-01   0.78881E-02 
c  VelocityY    0.70420E+08      41   0.15707E-01   0.49205E-02 
c  VelocityZ    0.70420E+08      41   0.15707E-01   0.10281E-01 
c  TurbEner     0.62130E+07     148   0.25995E-02   0.25070E-02 
c  Dissip       0.25747E+07      90   0.34086E-03   0.78203E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -0.0015013                           180


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69702           68860          3121.8            5609
v  Velocity[x]            -6.8475          6.5041       -0.012376       -0.018648
v  Velocity[y]            -8.9013           7.185        -0.01613       -0.012591
v  Velocity[z]            -10.825          2.5261          -3.149         -5.3335
v  TurbEner            0.00051911          6.8239         0.13265         0.21576
v  Dissip              3.5301e-11          5.0764        0.048764        0.079718
v  TurbVisc                1.2057      5.4507e+06          1960.9          1236.5
v  CourantNb                    0          2.8158         0.28236         0.45533
v  FourierNb           0.00068798          745.97         0.57365         0.34126
v  total_pressure           31623      1.7018e+05      1.0445e+05      1.0693e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014101          745.97         0.85601         0.79659


 TIME FOR THE TIME STEP               39:        0.24419E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.217200453E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.89993E+01
   Friction velocity        uet   :  0.00000E+00 0.34380E+00
   Friction velocity        uk    :  0.12479E-01 0.47114E+00
   Dimensionless distance   yplus :  0.13804E+04 0.20423E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24079E+05     271   0.15054E-02   0.76829E-01 
c  VelocityX    0.70428E+08      18   0.16407E-01   0.66140E-02 
c  VelocityY    0.70428E+08      18   0.16407E-01   0.42347E-02 
c  VelocityZ    0.70428E+08      18   0.16407E-01   0.11299E-01 
c  TurbEner     0.63383E+07      38   0.28588E-03   0.22923E-02 
c  Dissip       0.26401E+07     144   0.13584E-03   0.73393E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -4.0539e-06                           178


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68382           70140          3303.9          5910.7
v  Velocity[x]            -6.8497          6.5407        -0.01175       -0.017516
v  Velocity[y]            -8.8543          7.1763       -0.017138       -0.014755
v  Velocity[z]            -10.842          2.5489         -3.1489         -5.3332
v  TurbEner            0.00051728           6.798         0.13388         0.21835
v  Dissip              2.4991e-11          5.0055        0.049229        0.080832
v  TurbVisc                1.2031      9.5025e+05          1294.7          847.46
v  CourantNb                    0          2.8091         0.28236         0.45537
v  FourierNb           0.00068611          189.28         0.39202         0.23467
v  total_pressure           32943      1.7146e+05      1.0463e+05      1.0724e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014073          189.28         0.67438         0.69004


 TIME FOR THE TIME STEP               40:        0.25563E+00

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


 INSTANT    0.410000000E+01   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.243477380E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393703E+07
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 0.90140E+01
   Friction velocity        uet   :  0.00000E+00 0.34558E+00
   Friction velocity        uk    :  0.12457E-01 0.47746E+00
   Dimensionless distance   yplus :  0.13787E+04 0.20719E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25319E+05     309   0.16246E-02   0.80726E-01 
c  VelocityX    0.70688E+08     972   0.30301E-01   0.71740E-02 
c  VelocityY    0.70688E+08     972   0.30301E-01   0.68728E-02 
c  VelocityZ    0.70688E+08     972   0.30301E-01   0.10369E-01 
c  TurbEner     0.75657E+07    1178   0.10204E+01   0.14335E+00 
c  Dissip       0.27220E+07     845   0.62471E-02   0.62732E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip         -0.001857                           158


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68978           69578          3482.5          6203.9
v  Velocity[x]            -6.7726          6.5709       -0.011171       -0.016563
v  Velocity[y]            -8.8126          7.1208       -0.018314        -0.01725
v  Velocity[z]            -10.843          2.6085         -3.1485         -5.3327
v  TurbEner            0.00051546          6.8167         0.13815           0.226
v  Dissip               3.418e-12           4.987        0.049692        0.081929
v  TurbVisc                1.2006      2.8534e+06          1584.1          1513.2
v  CourantNb                    0          2.8124         0.28236         0.45538
v  FourierNb           0.00068476          244.59            0.43         0.33298
v  total_pressure           32347       1.709e+05      1.0481e+05      1.0753e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014046          244.59         0.71236         0.78836


 TIME FOR THE TIME STEP               41:        0.70492E+00

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


 INSTANT    0.420000000E+01   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.802893020E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.90034E+01
   Friction velocity        uet   :  0.00000E+00 0.34597E+00
   Friction velocity        uk    :  0.12435E-01 0.77786E+00
   Dimensionless distance   yplus :  0.13770E+04 0.30766E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24598E+05     283   0.15268E-02   0.78086E-01 
c  VelocityX    0.71360E+08     749   0.54644E-01   0.62147E-02 
c  VelocityY    0.71360E+08     749   0.54644E-01   0.55902E-02 
c  VelocityZ    0.71360E+08     749   0.54644E-01   0.10432E-01 
c  TurbEner     0.12008E+08     956   0.47047E+00   0.72359E-01 
c  Dissip       0.62481E+07    1034   0.13905E+00   0.52090E-02 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -4.231e-07                           182


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66767           70388          3554.7          6328.2
v  Velocity[x]            -6.8058          6.5875       -0.010474       -0.015319
v  Velocity[y]            -8.7967          7.1467       -0.019373       -0.019345
v  Velocity[z]            -10.841          2.6607         -3.1484         -5.3327
v  TurbEner            0.00051366          6.8136         0.14015         0.23008
v  Dissip              1.3854e-12          4.9341         0.05089        0.084348
v  TurbVisc                1.1981      9.8092e+06          2942.6          2705.4
v  CourantNb                    0          2.8082         0.28236         0.45539
v  FourierNb           0.00067845          1707.6         0.92482         0.69305
v  total_pressure           34558      1.7171e+05      1.0488e+05      1.0765e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014019          1707.6          1.2072          1.1484


 TIME FOR THE TIME STEP               42:        0.60027E+00

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


 INSTANT    0.430000000E+01   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.131792722E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393704E+07
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 0.90184E+01
   Friction velocity        uet   :  0.00000E+00 0.34674E+00
   Friction velocity        uk    :  0.12414E-01 0.72760E+00
   Dimensionless distance   yplus :  0.13753E+04 0.28778E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27598E+05     319   0.16260E-02   0.87988E-01 
c  VelocityX    0.70458E+08      17   0.17587E-01   0.84205E-02 
c  VelocityY    0.70458E+08      17   0.17587E-01   0.59796E-02 
c  VelocityZ    0.70458E+08      17   0.17587E-01   0.13423E-01 
c  TurbEner     0.67955E+07    6228   0.30032E-03   0.78334E-02 
c  Dissip       0.28393E+07    7766   0.18046E-03   0.87188E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.1442e-07                           163


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67131           70714          3803.3          6738.1
v  Velocity[x]            -6.8109          6.5377      -0.0097842       -0.014268
v  Velocity[y]            -8.8777          7.1104       -0.020395        -0.02133
v  Velocity[z]            -10.878          2.7105         -3.1484         -5.3328
v  TurbEner            0.00051187          6.8432         0.14121         0.23232
v  Dissip              7.0464e-11          4.8512        0.051306        0.085357
v  TurbVisc                1.1957      2.4197e+07          3927.5            3174
v  CourantNb                    0          2.8094         0.28234         0.45538
v  FourierNb           0.00067414          3980.7          1.3381          1.0113
v  total_pressure           34194      1.7204e+05      1.0513e+05      1.0806e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013993          3980.7          1.6205          1.4667


 TIME FOR THE TIME STEP               43:        0.11849E+01

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


 INSTANT    0.440000000E+01   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.192377875E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.90023E+01
   Friction velocity        uet   :  0.00000E+00 0.34721E+00
   Friction velocity        uk    :  0.12392E-01 0.70989E+00
   Dimensionless distance   yplus :  0.13736E+04 0.27479E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26717E+05     326   0.15615E-02   0.85098E-01 
c  VelocityX    0.70460E+08      17   0.16962E-01   0.75581E-02 
c  VelocityY    0.70460E+08      17   0.16962E-01   0.54163E-02 
c  VelocityZ    0.70460E+08      17   0.16962E-01   0.12176E-01 
c  TurbEner     0.69028E+07      19   0.21206E-03   0.50876E-02 
c  Dissip       0.28977E+07      19   0.12889E-03   0.69974E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.3125e-07                           156


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -70102           70318          3513.3          6256.1
v  Velocity[x]            -6.8558          6.5679      -0.0088479       -0.012566
v  Velocity[y]            -8.9217          7.1608       -0.020996       -0.022782
v  Velocity[z]            -10.903          2.7544         -3.1484         -5.3326
v  TurbEner             0.0005101          6.8706         0.14225         0.23451
v  Dissip              4.1381e-11          4.7849        0.051718        0.086339
v  TurbVisc                1.1933       4.756e+05          981.87          728.33
v  CourantNb                    0          2.8051          0.2823         0.45534
v  FourierNb           0.00067025          77.004         0.28873         0.19158
v  total_pressure           31223      1.7164e+05      1.0484e+05      1.0758e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013967          77.004         0.57103         0.64692


 TIME FOR THE TIME STEP               44:        0.21781E+00

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


 INSTANT    0.450000000E+01   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.887367883E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.90072E+01
   Friction velocity        uet   :  0.00000E+00 0.34818E+00
   Friction velocity        uk    :  0.12370E-01 0.68747E+00
   Dimensionless distance   yplus :  0.13720E+04 0.25685E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24728E+05     305   0.16691E-02   0.78719E-01 
c  VelocityX    0.70465E+08      17   0.16361E-01   0.54509E-02 
c  VelocityY    0.70465E+08      17   0.16361E-01   0.42757E-02 
c  VelocityZ    0.70465E+08      17   0.16361E-01   0.10615E-01 
c  TurbEner     0.70152E+07      59   0.16100E-03   0.38773E-02 
c  Dissip       0.29556E+07     115   0.10730E-03   0.59241E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.6922e-07                           182


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67539           70492          3762.2          6673.8
v  Velocity[x]             -6.864           6.519      -0.0083158       -0.011529
v  Velocity[y]            -8.8754          7.1349       -0.021834       -0.024371
v  Velocity[z]            -10.904          2.7927         -3.1482         -5.3324
v  TurbEner            0.00050834          6.9082         0.14322         0.23661
v  Dissip              3.4719e-11          4.7618        0.052098        0.087263
v  TurbVisc                1.1909      8.0926e+05            1145           917.8
v  CourantNb                    0          2.8017         0.28227          0.4553
v  FourierNb           0.00066707          154.06         0.35299         0.24682
v  total_pressure           33786      1.7182e+05      1.0509e+05        1.08e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013942          154.06         0.63526         0.70211


 TIME FOR THE TIME STEP               45:        0.21289E+00

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


 INSTANT    0.460000000E+01   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.709727569E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.89269E+01
   Friction velocity        uet   :  0.00000E+00 0.34764E+00
   Friction velocity        uk    :  0.12349E-01 0.65349E+00
   Dimensionless distance   yplus :  0.13703E+04 0.24409E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26909E+05     281   0.15635E-02   0.85416E-01 
c  VelocityX    0.70459E+08      18   0.17729E-01   0.81680E-02 
c  VelocityY    0.70459E+08      18   0.17729E-01   0.52173E-02 
c  VelocityZ    0.70459E+08      18   0.17729E-01   0.11646E-01 
c  TurbEner     0.71352E+07      72   0.14286E-03   0.36194E-02 
c  Dissip       0.30159E+07      65   0.11821E-03   0.68249E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.3634e-07                           180


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65714           71433            3902          6911.4
v  Velocity[x]            -6.7649          6.5592      -0.0074301       -0.010241
v  Velocity[y]            -8.8465          7.1299       -0.022687       -0.026032
v  Velocity[z]             -10.92          2.8179         -3.1485         -5.3328
v  TurbEner            0.00050659          6.9614         0.14422         0.23876
v  Dissip              9.8435e-12          4.7133        0.052519        0.088237
v  TurbVisc                1.1885      9.6596e+05          1257.4          904.01
v  CourantNb                    0          2.8042         0.28226         0.45528
v  FourierNb           0.00066449             103         0.35976          0.2384
v  total_pressure           35611      1.7276e+05      1.0523e+05      1.0824e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013917             103         0.64202         0.69367


 TIME FOR THE TIME STEP               46:        0.20624E+00

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


 INSTANT    0.470000000E+01   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.430024700E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.89451E+01
   Friction velocity        uet   :  0.00000E+00 0.34795E+00
   Friction velocity        uk    :  0.12328E-01 0.61224E+00
   Dimensionless distance   yplus :  0.13687E+04 0.23265E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25076E+05     268   0.16023E-02   0.79829E-01 
c  VelocityX    0.70468E+08      17   0.16593E-01   0.72116E-02 
c  VelocityY    0.70468E+08      17   0.16593E-01   0.65992E-02 
c  VelocityZ    0.70468E+08      17   0.16593E-01   0.10782E-01 
c  TurbEner     0.72543E+07    1105   0.11349E-03   0.30256E-02 
c  Dissip       0.30734E+07    1060   0.98026E-04   0.57171E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -5.3194e-07                           165


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65692           71758          3995.3          7068.1
v  Velocity[x]            -6.8193          6.4871      -0.0068976      -0.0092171
v  Velocity[y]            -8.8578          7.1533       -0.023324        -0.02741
v  Velocity[z]            -10.931            2.83         -3.1482         -5.3327
v  TurbEner            0.00050485           7.031         0.14514         0.24079
v  Dissip              2.0493e-11          4.6423        0.052895        0.089137
v  TurbVisc                1.1862      3.4071e+06          1434.8          1079.3
v  CourantNb                    0           2.801         0.28224         0.45525
v  FourierNb            0.0006624          662.54         0.49837         0.33176
v  total_pressure           35633      1.7308e+05      1.0532e+05      1.0839e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013893          662.54         0.78061         0.78701


 TIME FOR THE TIME STEP               47:        0.33822E+00

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


 INSTANT    0.480000000E+01   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.434194439E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393705E+07
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 0.89356E+01
   Friction velocity        uet   :  0.00000E+00 0.34754E+00
   Friction velocity        uk    :  0.12307E-01 0.59994E+00
   Dimensionless distance   yplus :  0.13670E+04 0.22799E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23880E+05     271   0.16098E-02   0.76192E-01 
c  VelocityX    0.70456E+08      17   0.18152E-01   0.68707E-02 
c  VelocityY    0.70456E+08      17   0.18152E-01   0.46224E-02 
c  VelocityZ    0.70456E+08      17   0.18152E-01   0.10545E-01 
c  TurbEner     0.73721E+07     139   0.92732E-04   0.26138E-02 
c  Dissip       0.31286E+07     159   0.83007E-04   0.49140E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.2061e-07                           172


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65224           71714          4003.2          7078.8
v  Velocity[x]            -6.8506          6.5003      -0.0062881      -0.0081737
v  Velocity[y]            -8.8351          7.1828       -0.023611        -0.02814
v  Velocity[z]            -10.978          2.8331         -3.1482         -5.3326
v  TurbEner            0.00050313          7.1095         0.14599         0.24274
v  Dissip              2.1846e-10          4.5733        0.053248        0.089987
v  TurbVisc                1.1838      1.6344e+06          1297.2          1095.1
v  CourantNb                    0          2.8054          0.2822         0.45521
v  FourierNb           0.00066055          195.65         0.39669         0.28544
v  total_pressure           36101      1.7304e+05      1.0533e+05       1.084e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001387          195.65         0.67889         0.74064


 TIME FOR THE TIME STEP               48:        0.23753E+00

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


 INSTANT    0.490000000E+01   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.283373962E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.89539E+01
   Friction velocity        uet   :  0.00000E+00 0.34892E+00
   Friction velocity        uk    :  0.12286E-01 0.57845E+00
   Dimensionless distance   yplus :  0.13654E+04 0.22905E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22946E+05     290   0.15772E-02   0.73459E-01 
c  VelocityX    0.70467E+08      17   0.18533E-01   0.59466E-02 
c  VelocityY    0.70467E+08      17   0.18533E-01   0.47490E-02 
c  VelocityZ    0.70467E+08      17   0.18533E-01   0.91929E-02 
c  TurbEner     0.74898E+07      18   0.82992E-04   0.23342E-02 
c  Dissip       0.31835E+07      18   0.77596E-04   0.43851E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.6736e-07                           155


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -64470           72441          4227.7          7455.7
v  Velocity[x]            -6.8011          6.4942      -0.0056182      -0.0071072
v  Velocity[y]             -8.792          7.1047       -0.024102       -0.029087
v  Velocity[z]            -10.937          2.8282         -3.1482         -5.3328
v  TurbEner            0.00050142          7.1967          0.1468         0.24459
v  Dissip              2.8346e-11          4.5517        0.053575        0.090791
v  TurbVisc                1.1816      1.5341e+05          859.02          639.44
v  CourantNb                    0          2.7996         0.28216         0.45515
v  FourierNb           0.00065918          29.379         0.26203         0.17209
v  total_pressure           36855      1.7377e+05      1.0555e+05      1.0878e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013847          29.379         0.54419         0.62724


 TIME FOR THE TIME STEP               49:        0.21023E+00

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


 INSTANT    0.500000000E+01   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.241427640E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.89344E+01
   Friction velocity        uet   :  0.00000E+00 0.34878E+00
   Friction velocity        uk    :  0.12265E-01 0.55895E+00
   Dimensionless distance   yplus :  0.13638E+04 0.23133E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12


 Write intermediate 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:    0.46087E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27542E+05     292   0.17863E-02   0.87944E-01 
c  VelocityX    0.70463E+08      17   0.17775E-01   0.55490E-02 
c  VelocityY    0.70463E+08      17   0.17775E-01   0.52291E-02 
c  VelocityZ    0.70463E+08      17   0.17775E-01   0.16502E-01 
c  TurbEner     0.76061E+07      23   0.75506E-04   0.21192E-02 
c  Dissip       0.32360E+07      56   0.72505E-04   0.40354E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.0169e-07                           158


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66151           72093          4151.7          7332.3
v  Velocity[x]            -6.7745          6.5556      -0.0049313      -0.0057216
v  Velocity[y]            -8.8878          7.0787       -0.024221       -0.029569
v  Velocity[z]            -10.935          2.8164         -3.1484         -5.3332
v  TurbEner            0.00049973          7.2852         0.14755         0.24636
v  Dissip              2.1946e-11           4.508        0.053879         0.09155
v  TurbVisc                1.1793      1.1798e+06          1205.5           939.5
v  CourantNb                    0          2.7967         0.28213          0.4551
v  FourierNb           0.00065792           149.8         0.38321         0.25778
v  total_pressure           35174      1.7342e+05      1.0548e+05      1.0866e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013825           149.8         0.66534         0.71288


 TIME FOR THE TIME STEP               50:        0.21593E+00

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


 INSTANT    0.510000000E+01   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.929997966E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.89380E+01
   Friction velocity        uet   :  0.00000E+00 0.33437E+00
   Friction velocity        uk    :  0.12244E-01 0.55883E+00
   Dimensionless distance   yplus :  0.13622E+04 0.23365E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24148E+05     293   0.16613E-02   0.76989E-01 
c  VelocityX    0.70472E+08      17   0.16788E-01   0.51731E-02 
c  VelocityY    0.70472E+08      17   0.16788E-01   0.33336E-02 
c  VelocityZ    0.70472E+08      17   0.16788E-01   0.11184E-01 
c  TurbEner     0.77209E+07     244   0.71395E-04   0.19388E-02 
c  Dissip       0.32875E+07     367   0.69879E-04   0.37734E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0095e-07                           156


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66881           72141          4235.8          7468.2
v  Velocity[x]            -6.7144          6.5047      -0.0043802      -0.0046977
v  Velocity[y]             -8.889          7.1471        -0.02424        -0.02988
v  Velocity[z]            -10.932          2.7982         -3.1484         -5.3333
v  TurbEner            0.00049805          7.3758         0.14824         0.24803
v  Dissip              3.4837e-11          4.4479        0.054157        0.092263
v  TurbVisc                1.1771      1.5249e+06          1102.2          837.92
v  CourantNb                    0          2.8011         0.28211         0.45506
v  FourierNb            0.0006569          253.26         0.35149         0.23882
v  total_pressure           34444      1.7347e+05      1.0556e+05      1.0879e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013803          253.26          0.6336         0.69389


 TIME FOR THE TIME STEP               51:        0.24333E+00

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


 INSTANT    0.520000000E+01   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.160243847E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88655E+01
   Friction velocity        uet   :  0.00000E+00 0.33473E+00
   Friction velocity        uk    :  0.12224E-01 0.57262E+00
   Dimensionless distance   yplus :  0.13606E+04 0.23590E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25016E+05     310   0.16088E-02   0.80255E-01 
c  VelocityX    0.70457E+08      17   0.17588E-01   0.83404E-02 
c  VelocityY    0.70457E+08      17   0.17588E-01   0.35528E-02 
c  VelocityZ    0.70457E+08      17   0.17588E-01   0.11767E-01 
c  TurbEner     0.78345E+07      18   0.67496E-04   0.17808E-02 
c  Dissip       0.33383E+07      50   0.66869E-04   0.34385E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0787e-07                           150


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67440           70859          4005.5          7083.5
v  Velocity[x]            -6.7903          6.5148      -0.0038426      -0.0038371
v  Velocity[y]            -8.8332          7.1105       -0.024079       -0.029974
v  Velocity[z]            -11.006          2.7765         -3.1481         -5.3329
v  TurbEner            0.00049638          7.4704          0.1489         0.24964
v  Dissip              5.1974e-11          4.4379        0.054424        0.092952
v  TurbVisc                1.1749      9.6148e+05            1035          811.59
v  CourantNb                    0          2.7961         0.28208         0.45501
v  FourierNb           0.00065575          136.91         0.31412         0.22027
v  total_pressure           33885      1.7218e+05      1.0533e+05      1.0841e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013782          136.91          0.5962         0.67528


 TIME FOR THE TIME STEP               52:        0.20991E+00

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


 INSTANT    0.530000000E+01   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.189921954E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.88646E+01
   Friction velocity        uet   :  0.00000E+00 0.33576E+00
   Friction velocity        uk    :  0.12203E-01 0.58726E+00
   Dimensionless distance   yplus :  0.13591E+04 0.23809E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24075E+05     302   0.15758E-02   0.77009E-01 
c  VelocityX    0.70444E+08      17   0.15522E-01   0.72519E-02 
c  VelocityY    0.70444E+08      17   0.15522E-01   0.48587E-02 
c  VelocityZ    0.70444E+08      17   0.15522E-01   0.99308E-02 
c  TurbEner     0.79452E+07      91   0.64004E-04   0.16271E-02 
c  Dissip       0.33870E+07     124   0.63422E-04   0.31372E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -1.712e-07                           157


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66616           71537          4171.3          7370.2
v  Velocity[x]            -6.8052          6.5176      -0.0034536      -0.0030781
v  Velocity[y]            -8.8411          7.1616       -0.024138       -0.030275
v  Velocity[z]            -10.975          2.7495         -3.1483         -5.3331
v  TurbEner            0.00049472          7.5654         0.14952         0.25115
v  Dissip              6.2768e-12          4.4108        0.054673        0.093592
v  TurbVisc                1.1727      6.4508e+05          988.95          748.55
v  CourantNb                    0          2.7932         0.28204         0.45494
v  FourierNb           0.00065506           92.82         0.30487         0.20458
v  total_pressure           34709      1.7286e+05       1.055e+05       1.087e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013762           92.82         0.58691         0.65951


 TIME FOR THE TIME STEP               53:        0.22394E+00

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


 INSTANT    0.540000000E+01   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.223024793E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88446E+01
   Friction velocity        uet   :  0.00000E+00 0.33795E+00
   Friction velocity        uk    :  0.12183E-01 0.60214E+00
   Dimensionless distance   yplus :  0.13575E+04 0.24210E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.21997E+05     308   0.14277E-02   0.70165E-01 
c  VelocityX    0.70452E+08      17   0.17941E-01   0.55132E-02 
c  VelocityY    0.70452E+08      17   0.17941E-01   0.42406E-02 
c  VelocityZ    0.70452E+08      17   0.17941E-01   0.90107E-02 
c  TurbEner     0.80519E+07      50   0.63089E-04   0.14708E-02 
c  Dissip       0.34327E+07      46   0.62818E-04   0.27924E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -8.2169e-07                           160


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66461           71956          4089.6          7234.3
v  Velocity[x]             -6.824          6.5647      -0.0027968        -0.00194
v  Velocity[y]            -8.9217          7.1531       -0.023951       -0.030106
v  Velocity[z]            -10.937          2.7154         -3.1487         -5.3335
v  TurbEner            0.00049308          7.6556         0.15009         0.25256
v  Dissip              4.7658e-12          4.3692        0.054896        0.094178
v  TurbVisc                1.1705       5.336e+06          1659.2          1110.5
v  CourantNb                    0          2.7982           0.282         0.45487
v  FourierNb           0.00068063          791.65         0.53937         0.30965
v  total_pressure           34864      1.7328e+05      1.0541e+05      1.0856e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013741          791.65         0.82136         0.76452


 TIME FOR THE TIME STEP               54:        0.21623E+00

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


 INSTANT    0.550000000E+01   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.277513601E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.88582E+01
   Friction velocity        uet   :  0.00000E+00 0.34221E+00
   Friction velocity        uk    :  0.12162E-01 0.61663E+00
   Dimensionless distance   yplus :  0.13559E+04 0.24792E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25318E+05     309   0.15522E-02   0.81196E-01 
c  VelocityX    0.70451E+08      18   0.15911E-01   0.67381E-02 
c  VelocityY    0.70451E+08      18   0.15911E-01   0.46037E-02 
c  VelocityZ    0.70451E+08      18   0.15911E-01   0.11836E-01 
c  TurbEner     0.81548E+07     623   0.58257E-04   0.13331E-02 
c  Dissip       0.34758E+07     526   0.56934E-04   0.24676E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.6477e-07                           145


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66651           71982          4209.2          7434.8
v  Velocity[x]            -6.8109          6.5122      -0.0026291      -0.0014593
v  Velocity[y]            -8.8913          7.1794       -0.023839       -0.030171
v  Velocity[z]            -10.958           2.678         -3.1486         -5.3336
v  TurbEner            0.00049144          7.7459         0.15062         0.25388
v  Dissip              1.8604e-11          4.4346        0.055097        0.094714
v  TurbVisc                1.1684      7.0422e+06          2292.3          1542.7
v  CourantNb                    0          2.7926         0.28197         0.45481
v  FourierNb           0.00065392          829.03         0.64943         0.41458
v  total_pressure           34674      1.7331e+05      1.0553e+05      1.0876e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013721          829.03          0.9314          0.8694


 TIME FOR THE TIME STEP               55:        0.29381E+00

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


 INSTANT    0.560000000E+01   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.533343388E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.88356E+01
   Friction velocity        uet   :  0.00000E+00 0.34492E+00
   Friction velocity        uk    :  0.12142E-01 0.63026E+00
   Dimensionless distance   yplus :  0.13544E+04 0.25340E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23648E+05     304   0.14337E-02   0.75795E-01 
c  VelocityX    0.70440E+08      17   0.15717E-01   0.55175E-02 
c  VelocityY    0.70440E+08      17   0.15717E-01   0.57064E-02 
c  VelocityZ    0.70440E+08      17   0.15717E-01   0.79430E-02 
c  TurbEner     0.82548E+07      18   0.55686E-04   0.12150E-02 
c  Dissip       0.35180E+07     254   0.55148E-04   0.21941E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.4966e-07                           165


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65939           71934          4083.7            7227
v  Velocity[x]            -6.8606          6.5533      -0.0022803     -0.00080036
v  Velocity[y]            -8.8683           7.128       -0.023473        -0.02967
v  Velocity[z]            -11.019          2.6373         -3.1488         -5.3337
v  TurbEner            0.00048982          7.8341         0.15113         0.25513
v  Dissip              6.9969e-11           4.498        0.055301        0.095228
v  TurbVisc                1.1663       1.799e+06          1346.4          1012.5
v  CourantNb                    0          2.7902         0.28193         0.45476
v  FourierNb           0.00065332          291.78          0.4038         0.27361
v  total_pressure           35386      1.7326e+05      1.0541e+05      1.0855e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013702          291.78         0.68574         0.72837


 TIME FOR THE TIME STEP               56:        0.23154E+00

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


 INSTANT    0.570000000E+01   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.217353283E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.88398E+01
   Friction velocity        uet   :  0.00000E+00 0.34805E+00
   Friction velocity        uk    :  0.12122E-01 0.64278E+00
   Dimensionless distance   yplus :  0.13529E+04 0.25843E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22469E+05     268   0.13285E-02   0.71854E-01 
c  VelocityX    0.70443E+08      17   0.16220E-01   0.65408E-02 
c  VelocityY    0.70443E+08      17   0.16220E-01   0.44489E-02 
c  VelocityZ    0.70443E+08      17   0.16220E-01   0.87735E-02 
c  TurbEner     0.83501E+07      53   0.53740E-04   0.10931E-02 
c  Dissip       0.35570E+07      63   0.52953E-04   0.19036E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.4156e-07                           143


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -64776           72898          4087.6          7239.1
v  Velocity[x]            -6.8904           6.547      -0.0019033     -0.00024705
v  Velocity[y]             -8.844           7.184       -0.023219       -0.029384
v  Velocity[z]            -10.984          2.5951         -3.1489         -5.3338
v  TurbEner            0.00048821          7.9149         0.15159         0.25627
v  Dissip              2.2226e-11           4.555        0.055471        0.095681
v  TurbVisc                1.1642      4.7927e+05          949.96          739.23
v  CourantNb                    0          2.7952         0.28191         0.45471
v  FourierNb           0.00068014          55.535          0.2818         0.19325
v  total_pressure           36549      1.7422e+05      1.0541e+05      1.0856e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013682          55.535         0.56371         0.64795


 TIME FOR THE TIME STEP               57:        0.21184E+00

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


 INSTANT    0.580000000E+01   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.821408062E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393705E+07
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 0.88049E+01
   Friction velocity        uet   :  0.00000E+00 0.34925E+00
   Friction velocity        uk    :  0.12102E-01 0.65385E+00
   Dimensionless distance   yplus :  0.13513E+04 0.26289E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22874E+05     266   0.14312E-02   0.73187E-01 
c  VelocityX    0.70447E+08      17   0.16217E-01   0.66948E-02 
c  VelocityY    0.70447E+08      17   0.16217E-01   0.41822E-02 
c  VelocityZ    0.70447E+08      17   0.16217E-01   0.99105E-02 
c  TurbEner     0.84410E+07      66   0.49459E-04   0.99082E-03 
c  Dissip       0.35934E+07      63   0.47790E-04   0.16799E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.3435e-07                           152


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67645           72591          4166.2            7368
v  Velocity[x]            -6.8907          6.6084      -0.0015957      0.00032707
v  Velocity[y]            -8.8578          7.1839       -0.022566       -0.028501
v  Velocity[z]            -10.968          2.5512         -3.1494         -5.3344
v  TurbEner            0.00048662          7.9961         0.15204         0.25735
v  Dissip              9.6376e-11          4.6123        0.055637          0.0961
v  TurbVisc                1.1622      1.5055e+06          1239.7          957.19
v  CourantNb                    0          2.7904         0.28189         0.45466
v  FourierNb           0.00065246          242.51         0.39365         0.26646
v  total_pressure           33680      1.7392e+05      1.0549e+05      1.0869e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013663          242.51         0.67554         0.72113


 TIME FOR THE TIME STEP               58:        0.20449E+00

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


 INSTANT    0.590000000E+01   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.137182401E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393703E+07
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 0.88069E+01
   Friction velocity        uet   :  0.00000E+00 0.35092E+00
   Friction velocity        uk    :  0.12082E-01 0.66312E+00
   Dimensionless distance   yplus :  0.13498E+04 0.26661E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25790E+05     270   0.16582E-02   0.82635E-01 
c  VelocityX    0.70449E+08      18   0.16936E-01   0.76382E-02 
c  VelocityY    0.70449E+08      18   0.16936E-01   0.35632E-02 
c  VelocityZ    0.70449E+08      18   0.16936E-01   0.98354E-02 
c  TurbEner     0.85277E+07      17   0.48328E-04   0.90747E-03 
c  Dissip       0.36274E+07      17   0.47589E-04   0.14975E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -9.8707e-08                           149


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66393           72395          4129.4          7308.4
v  Velocity[x]            -6.9492          6.5757       -0.001366      0.00081835
v  Velocity[y]            -8.8057          7.1504       -0.022247       -0.027973
v  Velocity[z]             -10.96          2.5055         -3.1495         -5.3346
v  TurbEner            0.00048503          8.0725         0.15246         0.25836
v  Dissip              1.3076e-11          4.6652        0.055783        0.096482
v  TurbVisc                1.1601      3.4762e+05          955.13          702.73
v  CourantNb                    0          2.7886         0.28186         0.45461
v  FourierNb           0.00065214          58.711         0.28611         0.18803
v  total_pressure           34932      1.7372e+05      1.0545e+05      1.0863e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013645          58.711         0.56797         0.64264


 TIME FOR THE TIME STEP               59:        0.21180E+00

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


 INSTANT    0.600000000E+01   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.273381366E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.88514E+01
   Friction velocity        uet   :  0.00000E+00 0.35234E+00
   Friction velocity        uk    :  0.12063E-01 0.67037E+00
   Dimensionless distance   yplus :  0.13483E+04 0.26953E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25058E+05     294   0.15660E-02   0.80432E-01 
c  VelocityX    0.70437E+08      17   0.17847E-01   0.58926E-02 
c  VelocityY    0.70437E+08      17   0.17847E-01   0.38540E-02 
c  VelocityZ    0.70437E+08      17   0.17847E-01   0.11827E-01 
c  TurbEner     0.86094E+07      97   0.46506E-04   0.81685E-03 
c  Dissip       0.36583E+07      62   0.45252E-04   0.12702E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.2236e-07                           159


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65825           72130          3976.7          7055.2
v  Velocity[x]            -6.9816           6.602      -0.0010961       0.0012016
v  Velocity[y]            -8.8157          7.1234       -0.021632       -0.026911
v  Velocity[z]            -11.054           2.461         -3.1498         -5.3347
v  TurbEner            0.00048346          8.1433         0.15285         0.25928
v  Dissip              9.0923e-12          4.7131        0.055914        0.096816
v  TurbVisc                1.1581      2.5609e+06          1843.3            1397
v  CourantNb                    0          2.7936         0.28183         0.45456
v  FourierNb           0.00065167          324.28         0.51391         0.35521
v  total_pressure           35500      1.7346e+05       1.053e+05      1.0838e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013626          324.28         0.79575         0.80977


 TIME FOR THE TIME STEP               60:        0.22634E+00

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


 INSTANT    0.610000000E+01   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.166866622E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.88815E+01
   Friction velocity        uet   :  0.00000E+00 0.35250E+00
   Friction velocity        uk    :  0.12043E-01 0.67555E+00
   Dimensionless distance   yplus :  0.13468E+04 0.27161E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24888E+05     295   0.14618E-02   0.79532E-01 
c  VelocityX    0.70434E+08      17   0.19813E-01   0.51085E-02 
c  VelocityY    0.70434E+08      17   0.19813E-01   0.41429E-02 
c  VelocityZ    0.70434E+08      17   0.19813E-01   0.13641E-01 
c  TurbEner     0.86883E+07     105   0.45754E-04   0.77102E-03 
c  Dissip       0.36883E+07     520   0.45835E-04   0.12242E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.6089e-07                           156


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65383           72316            4053          7180.4
v  Velocity[x]            -6.9183           6.623      -0.0010708       0.0013943
v  Velocity[y]             -8.794          7.1537        -0.02092       -0.025967
v  Velocity[z]            -11.034          2.4193         -3.1499         -5.3349
v  TurbEner            0.00048189          8.2155         0.15324         0.26016
v  Dissip              3.1756e-11          4.7616        0.056044        0.097128
v  TurbVisc                1.1561      3.6837e+06          1628.4          1062.6
v  CourantNb                    0          2.7884         0.28181         0.45451
v  FourierNb           0.00065157          679.57         0.50612         0.30137
v  total_pressure           35942      1.7364e+05      1.0538e+05      1.0851e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013607          679.57         0.78793         0.75589


 TIME FOR THE TIME STEP               61:        0.25056E+00

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


 INSTANT    0.620000000E+01   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.222013753E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88874E+01
   Friction velocity        uet   :  0.00000E+00 0.35340E+00
   Friction velocity        uk    :  0.12024E-01 0.67882E+00
   Dimensionless distance   yplus :  0.13454E+04 0.27292E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24980E+05     296   0.15168E-02   0.79492E-01 
c  VelocityX    0.70425E+08      17   0.19498E-01   0.78957E-02 
c  VelocityY    0.70425E+08      17   0.19498E-01   0.37215E-02 
c  VelocityZ    0.70425E+08      17   0.19498E-01   0.98372E-02 
c  TurbEner     0.87637E+07      71   0.43298E-04   0.71569E-03 
c  Dissip       0.37168E+07      73   0.43263E-04   0.11076E-03 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -7.4984e-08                           170


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67640           71150          3920.2          6960.5
v  Velocity[x]            -6.9171          6.6676     -0.00098043       0.0015604
v  Velocity[y]             -8.835           7.147       -0.020331       -0.025043
v  Velocity[z]            -11.025          2.3779         -3.1501         -5.3348
v  TurbEner            0.00048034          8.2838         0.15363           0.261
v  Dissip              8.4595e-11          4.8067        0.056181        0.097429
v  TurbVisc                1.1542       1.053e+06            1100          852.69
v  CourantNb                    0          2.7876          0.2818         0.45448
v  FourierNb           0.00065045          124.53         0.33711         0.22691
v  total_pressure           33685      1.7248e+05      1.0525e+05      1.0829e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001359          124.53         0.61891         0.68139


 TIME FOR THE TIME STEP               62:        0.22035E+00

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


 INSTANT    0.630000000E+01   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.272615680E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.88952E+01
   Friction velocity        uet   :  0.00000E+00 0.35382E+00
   Friction velocity        uk    :  0.12004E-01 0.68024E+00
   Dimensionless distance   yplus :  0.13439E+04 0.27350E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27787E+05     295   0.16089E-02   0.88371E-01 
c  VelocityX    0.70424E+08      17   0.17180E-01   0.72163E-02 
c  VelocityY    0.70424E+08      17   0.17180E-01   0.33755E-02 
c  VelocityZ    0.70424E+08      17   0.17180E-01   0.16628E-01 
c  TurbEner     0.88351E+07      17   0.42252E-04   0.65709E-03 
c  Dissip       0.37429E+07      17   0.41443E-04   0.97740E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -7.8152e-08                           135


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68313           72257          3960.5          7032.6
v  Velocity[x]            -6.9498          6.6089      -0.0010088       0.0015388
v  Velocity[y]            -8.8417          7.1924       -0.019727       -0.024103
v  Velocity[z]            -11.034          2.3389           -3.15         -5.3351
v  TurbEner            0.00047875          8.3504           0.154         0.26178
v  Dissip              1.8502e-11          4.8501        0.056299        0.097691
v  TurbVisc                1.1522      3.9644e+05          1031.4          751.68
v  CourantNb                    0          2.7929         0.28177         0.45444
v  FourierNb           0.00065109          46.469         0.30514         0.19992
v  total_pressure           33012      1.7358e+05      1.0529e+05      1.0836e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013572          46.469         0.58691         0.65435


 TIME FOR THE TIME STEP               63:        0.22196E+00

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


 INSTANT    0.640000000E+01   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.109752650E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88925E+01
   Friction velocity        uet   :  0.00000E+00 0.33850E+00
   Friction velocity        uk    :  0.11984E-01 0.67997E+00
   Dimensionless distance   yplus :  0.13424E+04 0.27339E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24629E+05     270   0.15762E-02   0.78650E-01 
c  VelocityX    0.70421E+08      17   0.16371E-01   0.58855E-02 
c  VelocityY    0.70421E+08      17   0.16371E-01   0.44064E-02 
c  VelocityZ    0.70421E+08      17   0.16371E-01   0.11389E-01 
c  TurbEner     0.89022E+07      43   0.39495E-04   0.60097E-03 
c  Dissip       0.37660E+07      20   0.37655E-04   0.84225E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0595e-07                           142


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68353           71856          3911.6          6952.6
v  Velocity[x]             -6.866           6.631     -0.00095315       0.0016956
v  Velocity[y]            -8.9292          7.1564       -0.018956       -0.022933
v  Velocity[z]            -11.123          2.3008         -3.1503         -5.3353
v  TurbEner            0.00047713          8.4177         0.15436         0.26253
v  Dissip              1.1959e-11           4.894        0.056403        0.097928
v  TurbVisc                1.1503      1.8101e+06          1157.3          848.83
v  CourantNb                    0          2.7888         0.28175         0.45441
v  FourierNb            0.0006508          217.81         0.34137         0.22365
v  total_pressure           32972      1.7318e+05      1.0524e+05      1.0828e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013555          217.81         0.62312         0.67806


 TIME FOR THE TIME STEP               64:        0.20887E+00

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


 INSTANT    0.650000000E+01   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.394010242E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393704E+07
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 0.88880E+01
   Friction velocity        uet   :  0.00000E+00 0.33878E+00
   Friction velocity        uk    :  0.11964E-01 0.67824E+00
   Dimensionless distance   yplus :  0.13410E+04 0.27269E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23091E+05     273   0.14266E-02   0.73642E-01 
c  VelocityX    0.70426E+08      17   0.16449E-01   0.55767E-02 
c  VelocityY    0.70426E+08      17   0.16449E-01   0.34269E-02 
c  VelocityZ    0.70426E+08      17   0.16449E-01   0.10682E-01 
c  TurbEner     0.89659E+07     233   0.37381E-04   0.57118E-03 
c  Dissip       0.37871E+07      40   0.34962E-04   0.78742E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.3544e-07                           143


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67978           71271          3874.2          6889.3
v  Velocity[x]            -6.8932          6.6544      -0.0010158       0.0016453
v  Velocity[y]            -8.8925           7.196       -0.018412        -0.02197
v  Velocity[z]            -11.087          2.2627         -3.1502         -5.3353
v  TurbEner            0.00047551           8.485         0.15473         0.26326
v  Dissip              3.8122e-11          4.9378        0.056516        0.098154
v  TurbVisc                1.1484      2.8012e+06          1722.1            1152
v  CourantNb                    0           2.794         0.28173         0.45437
v  FourierNb           0.00065066          628.36          0.5692         0.34685
v  total_pressure           33347       1.726e+05       1.052e+05      1.0821e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013538          628.36         0.85093         0.80123


 TIME FOR THE TIME STEP               65:        0.22163E+00

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


 INSTANT    0.660000000E+01   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.250512665E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.88773E+01
   Friction velocity        uet   :  0.00000E+00 0.33953E+00
   Friction velocity        uk    :  0.11944E-01 0.67522E+00
   Dimensionless distance   yplus :  0.13396E+04 0.27148E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24721E+05     258   0.14638E-02   0.78557E-01 
c  VelocityX    0.70419E+08      17   0.17446E-01   0.75321E-02 
c  VelocityY    0.70419E+08      17   0.17446E-01   0.35324E-02 
c  VelocityZ    0.70419E+08      17   0.17446E-01   0.99086E-02 
c  TurbEner     0.90268E+07      17   0.35303E-04   0.52394E-03 
c  Dissip       0.38067E+07      20   0.32343E-04   0.69500E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.6456e-07                           144


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65775           71810          3911.5          6952.9
v  Velocity[x]              -6.85          6.7072     -0.00087089        0.001842
v  Velocity[y]            -8.8431          7.1813       -0.017735       -0.020818
v  Velocity[z]            -11.078          2.2231         -3.1505         -5.3356
v  TurbEner            0.00047391          8.5532         0.15509         0.26396
v  Dissip              2.9028e-11           4.982        0.056622        0.098364
v  TurbVisc                1.1465      8.7877e+05          1156.4          891.54
v  CourantNb                    0          2.7911         0.28172         0.45435
v  FourierNb           0.00065046          117.19         0.34653         0.23788
v  total_pressure           35550      1.7314e+05      1.0524e+05      1.0828e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013521          117.19         0.62825         0.69222


 TIME FOR THE TIME STEP               66:        0.19419E+00

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


 INSTANT    0.670000000E+01   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.152377724E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.88553E+01
   Friction velocity        uet   :  0.00000E+00 0.34209E+00
   Friction velocity        uk    :  0.11924E-01 0.67103E+00
   Dimensionless distance   yplus :  0.13381E+04 0.26980E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26352E+05     293   0.17294E-02   0.84128E-01 
c  VelocityX    0.70416E+08      17   0.14913E-01   0.75788E-02 
c  VelocityY    0.70416E+08      17   0.14913E-01   0.37685E-02 
c  VelocityZ    0.70416E+08      17   0.14913E-01   0.11070E-01 
c  TurbEner     0.90873E+07      40   0.38044E-04   0.56738E-03 
c  Dissip       0.38253E+07      43   0.35694E-04   0.80357E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -2.613e-07                           146


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69062           71477          3945.5          7009.5
v  Velocity[x]            -6.8404          6.6251     -0.00093687       0.0019257
v  Velocity[y]            -8.8523           7.182       -0.017091       -0.019905
v  Velocity[z]             -11.06          2.1831         -3.1504         -5.3354
v  TurbEner            0.00047231          8.6165         0.15547         0.26469
v  Dissip              2.7624e-11          5.0221        0.056727         0.09858
v  TurbVisc                1.1447      1.1533e+06          1224.2          858.32
v  CourantNb                    0          2.7873          0.2817         0.45433
v  FourierNb           0.00064967          377.45         0.39174         0.24316
v  total_pressure           32263       1.728e+05      1.0527e+05      1.0833e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013504          377.45         0.67345         0.69749


 TIME FOR THE TIME STEP               67:        0.20436E+00

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


 INSTANT    0.680000000E+01   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.166635418E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.88392E+01
   Friction velocity        uet   :  0.00000E+00 0.34568E+00
   Friction velocity        uk    :  0.11903E-01 0.66600E+00
   Dimensionless distance   yplus :  0.13367E+04 0.26777E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.21937E+05     307   0.14688E-02   0.69976E-01 
c  VelocityX    0.70416E+08      17   0.16427E-01   0.51778E-02 
c  VelocityY    0.70416E+08      17   0.16427E-01   0.36759E-02 
c  VelocityZ    0.70416E+08      17   0.16427E-01   0.89742E-02 
c  TurbEner     0.91457E+07      79   0.34423E-04   0.51550E-03 
c  Dissip       0.38436E+07      21   0.32918E-04   0.71731E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.7115e-07                           137


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67626           71151          3857.4          6864.8
v  Velocity[x]            -6.9609          6.6438     -0.00092312       0.0020402
v  Velocity[y]            -8.8874          7.1321       -0.016479       -0.018805
v  Velocity[z]            -11.101          2.1471         -3.1505         -5.3356
v  TurbEner            0.00047072          8.6799         0.15586         0.26541
v  Dissip              3.3626e-12          5.0623        0.056844        0.098794
v  TurbVisc                1.1428      1.2099e+06          1002.1          819.09
v  CourantNb                    0          2.7942         0.28169          0.4543
v  FourierNb           0.00065023          156.29         0.31007         0.21744
v  total_pressure           33699      1.7248e+05      1.0518e+05      1.0819e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013487          156.29         0.59176         0.67174


 TIME FOR THE TIME STEP               68:        0.20691E+00

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


 INSTANT    0.690000000E+01   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.106009424E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.88276E+01
   Friction velocity        uet   :  0.00000E+00 0.34820E+00
   Friction velocity        uk    :  0.11883E-01 0.66023E+00
   Dimensionless distance   yplus :  0.13353E+04 0.26545E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23677E+05     256   0.14565E-02   0.75367E-01 
c  VelocityX    0.70414E+08      17   0.16355E-01   0.69787E-02 
c  VelocityY    0.70414E+08      17   0.16355E-01   0.37358E-02 
c  VelocityZ    0.70414E+08      17   0.16355E-01   0.90594E-02 
c  TurbEner     0.92013E+07     221   0.33158E-04   0.46440E-03 
c  Dissip       0.38604E+07      17   0.31933E-04   0.60934E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.5492e-07                           113


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68473           71264          3841.5          6835.5
v  Velocity[x]            -6.9786          6.6414      -0.0010184       0.0018823
v  Velocity[y]            -8.9344          7.1521        -0.01594       -0.017845
v  Velocity[z]            -11.092          2.1149         -3.1506         -5.3354
v  TurbEner            0.00046914          8.7441         0.15624         0.26611
v  Dissip              5.4379e-11          5.1036        0.056955        0.098996
v  TurbVisc                 1.141      9.9584e+06            2235          1474.2
v  CourantNb                    0          2.7917         0.28167         0.45427
v  FourierNb           0.00065031            1045         0.54563         0.35075
v  total_pressure           32852      1.7259e+05      1.0517e+05      1.0816e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013471            1045          0.8273         0.80501


 TIME FOR THE TIME STEP               69:        0.21135E+00

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


 INSTANT    0.700000000E+01   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.173704383E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.88150E+01
   Friction velocity        uet   :  0.00000E+00 0.35094E+00
   Friction velocity        uk    :  0.11863E-01 0.65406E+00
   Dimensionless distance   yplus :  0.13339E+04 0.26297E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25063E+05     241   0.15470E-02   0.79980E-01 
c  VelocityX    0.70411E+08      17   0.16473E-01   0.64411E-02 
c  VelocityY    0.70411E+08      17   0.16473E-01   0.47046E-02 
c  VelocityZ    0.70411E+08      17   0.16473E-01   0.94960E-02 
c  TurbEner     0.92548E+07      24   0.32742E-04   0.43241E-03 
c  Dissip       0.38762E+07      28   0.32897E-04   0.57953E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0596e-07                           136


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67467           71653          3843.4          6841.3
v  Velocity[x]            -6.8711          6.6911     -0.00089275       0.0020461
v  Velocity[y]            -8.8809          7.1098        -0.01535       -0.016855
v  Velocity[z]            -11.042          2.0864         -3.1509         -5.3357
v  TurbEner            0.00046757          8.8077         0.15663          0.2668
v  Dissip              1.9287e-10          5.1444        0.057067        0.099191
v  TurbVisc                1.1392      6.1659e+05          978.67          794.26
v  CourantNb                    0          2.7956         0.28165         0.45423
v  FourierNb           0.00065028          83.178         0.28977         0.20612
v  total_pressure           33858      1.7298e+05      1.0517e+05      1.0817e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013455          83.178         0.57142         0.66035


 TIME FOR THE TIME STEP               70:        0.19521E+00

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


 INSTANT    0.710000000E+01   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.154222836E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393702E+07
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 0.88050E+01
   Friction velocity        uet   :  0.00000E+00 0.35236E+00
   Friction velocity        uk    :  0.11844E-01 0.64753E+00
   Dimensionless distance   yplus :  0.13325E+04 0.26303E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23615E+05     269   0.14556E-02   0.75257E-01 
c  VelocityX    0.70425E+08      17   0.15211E-01   0.50621E-02 
c  VelocityY    0.70425E+08      17   0.15211E-01   0.30178E-02 
c  VelocityZ    0.70425E+08      17   0.15211E-01   0.10726E-01 
c  TurbEner     0.93058E+07      17   0.32343E-04   0.41401E-03 
c  Dissip       0.38906E+07      16   0.33179E-04   0.56645E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -7.4155e-08                           131


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67100           71477          3814.6          6791.3
v  Velocity[x]             -6.957          6.6417        -0.00088       0.0020357
v  Velocity[y]            -8.8593          7.1575       -0.014919       -0.016229
v  Velocity[z]            -11.073          2.0627         -3.1508         -5.3356
v  TurbEner            0.00046601          8.8688         0.15703         0.26747
v  Dissip              5.7679e-11          5.1826         0.05718        0.099374
v  TurbVisc                1.1375      1.7334e+05          759.33          586.58
v  CourantNb                    0           2.793         0.28163         0.45421
v  FourierNb           0.00065027           39.21         0.23267         0.15725
v  total_pressure           34225       1.728e+05      1.0514e+05      1.0812e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013439           39.21         0.51431         0.61146


 TIME FOR THE TIME STEP               71:        0.20808E+00

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


 INSTANT    0.720000000E+01   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.382208337E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.87756E+01
   Friction velocity        uet   :  0.00000E+00 0.35309E+00
   Friction velocity        uk    :  0.11824E-01 0.64074E+00
   Dimensionless distance   yplus :  0.13312E+04 0.26367E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24061E+05     287   0.14114E-02   0.76776E-01 
c  VelocityX    0.70407E+08      17   0.18405E-01   0.59912E-02 
c  VelocityY    0.70407E+08      17   0.18405E-01   0.32318E-02 
c  VelocityZ    0.70407E+08      17   0.18405E-01   0.10787E-01 
c  TurbEner     0.93553E+07      43   0.29685E-04   0.38033E-03 
c  Dissip       0.39039E+07      52   0.29962E-04   0.48642E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -7.5645e-08                           132


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65724           71781          3789.9            6754
v  Velocity[x]            -6.9752          6.6809     -0.00074192        0.002051
v  Velocity[y]             -8.859          7.1273       -0.014521       -0.015384
v  Velocity[z]            -11.124          2.0435         -3.1512         -5.3359
v  TurbEner            0.00046445          8.9206         0.15743         0.26814
v  Dissip              3.1582e-13          5.2125        0.057292        0.099555
v  TurbVisc                1.1357      5.8096e+05          1121.5          851.88
v  CourantNb                    0          2.7908         0.28163          0.4542
v  FourierNb           0.00065017          74.704         0.33649         0.22738
v  total_pressure           35601      1.7311e+05      1.0511e+05      1.0808e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013423          74.704         0.61812         0.68157


 TIME FOR THE TIME STEP               72:        0.20823E+00

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


 INSTANT    0.730000000E+01   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.116763275E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.87482E+01
   Friction velocity        uet   :  0.00000E+00 0.35349E+00
   Friction velocity        uk    :  0.11804E-01 0.63392E+00
   Dimensionless distance   yplus :  0.13298E+04 0.26424E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24688E+05     278   0.17715E-02   0.78992E-01 
c  VelocityX    0.70410E+08      18   0.19786E-01   0.83534E-02 
c  VelocityY    0.70410E+08      18   0.19786E-01   0.38360E-02 
c  VelocityZ    0.70410E+08      18   0.19786E-01   0.10983E-01 
c  TurbEner     0.94034E+07   10000   0.29048E-04   0.35758E-03 
c  Dissip       0.39169E+07   10000   0.30425E-04   0.46781E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.1256e-07                           141


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65922           71232          3822.9          6804.9
v  Velocity[x]            -6.9635          6.6613     -0.00091958       0.0018272
v  Velocity[y]            -8.8494          7.1633       -0.014137         -0.0149
v  Velocity[z]            -11.077          2.0354         -3.1511         -5.3359
v  TurbEner            0.00046291          8.9751         0.15782         0.26879
v  Dissip              2.5226e-11          5.2447        0.057403        0.099729
v  TurbVisc                 1.134      1.0593e+08           14759          7257.6
v  CourantNb                    0           2.795         0.28163         0.45418
v  FourierNb           0.00065018           22700          5.6265          2.9096
v  total_pressure           35403      1.7256e+05      1.0515e+05      1.0813e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013407           22700          5.9081          3.3637


 TIME FOR THE TIME STEP               73:        0.15710E+01

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


 INSTANT    0.740000000E+01   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.143595761E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.87116E+01
   Friction velocity        uet   :  0.00000E+00 0.35370E+00
   Friction velocity        uk    :  0.11784E-01 0.62722E+00
   Dimensionless distance   yplus :  0.13284E+04 0.26468E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26888E+05     279   0.18245E-02   0.85665E-01 
c  VelocityX    0.70397E+08      17   0.17780E-01   0.63644E-02 
c  VelocityY    0.70397E+08      17   0.17780E-01   0.34669E-02 
c  VelocityZ    0.70397E+08      17   0.17780E-01   0.17361E-01 
c  TurbEner     0.94514E+07      59   0.30655E-04   0.36413E-03 
c  Dissip       0.39306E+07      48   0.34417E-04   0.53658E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.2887e-07                           132


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69509           72105          3875.2          6894.9
v  Velocity[x]            -6.9873          6.6594      -0.0010779       0.0015483
v  Velocity[y]            -9.0285          7.1614        -0.01364       -0.014001
v  Velocity[z]            -11.073          2.0255         -3.1513         -5.3361
v  TurbEner            0.00046137          9.0264         0.15823         0.26946
v  Dissip              1.0695e-11          5.2741        0.057526        0.099914
v  TurbVisc                1.1322      1.3288e+06          1124.5          845.66
v  CourantNb                    0          2.7929          0.2816         0.45414
v  FourierNb           0.00065013           163.4         0.34005         0.22985
v  total_pressure           31816      1.7343e+05       1.052e+05      1.0822e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013392           163.4         0.62165           0.684


 TIME FOR THE TIME STEP               74:        0.20633E+00

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


 INSTANT    0.750000000E+01   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.243925812E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.86758E+01
   Friction velocity        uet   :  0.00000E+00 0.33976E+00
   Friction velocity        uk    :  0.11765E-01 0.62058E+00
   Dimensionless distance   yplus :  0.13271E+04 0.26512E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12


 Write intermediate restart files
   checkpoint at iteration         75, Physical time    0.75000E+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:    0.46785E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24913E+05     245   0.16256E-02   0.79362E-01 
c  VelocityX    0.70402E+08      17   0.16729E-01   0.72434E-02 
c  VelocityY    0.70402E+08      17   0.16729E-01   0.37137E-02 
c  VelocityZ    0.70402E+08      17   0.16729E-01   0.97787E-02 
c  TurbEner     0.94994E+07      93   0.30439E-04   0.34757E-03 
c  Dissip       0.39449E+07      49   0.34435E-04   0.50945E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.1471e-07                           133


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -71089           71507          3829.8            6820
v  Velocity[x]             -6.889          6.6695      -0.0011622       0.0011856
v  Velocity[y]            -9.0295          7.1436       -0.013343       -0.013516
v  Velocity[z]            -11.045          2.0154         -3.1513         -5.3362
v  TurbEner            0.00045984          9.0774         0.15864         0.27012
v  Dissip              4.2255e-11          5.3028        0.057642          0.1001
v  TurbVisc                1.1305      3.1302e+06          1605.1          1241.3
v  CourantNb                    0          2.7975          0.2816         0.45413
v  FourierNb           0.00065014          328.61         0.43572          0.3076
v  total_pressure           30236      1.7283e+05      1.0515e+05      1.0815e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013376          328.61         0.71732         0.76173


 TIME FOR THE TIME STEP               75:        0.20801E+00

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


 INSTANT    0.760000000E+01   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.730998302E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393705E+07
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 0.86565E+01
   Friction velocity        uet   :  0.00000E+00 0.34100E+00
   Friction velocity        uk    :  0.11745E-01 0.61408E+00
   Dimensionless distance   yplus :  0.13258E+04 0.26533E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22897E+05     259   0.14979E-02   0.73014E-01 
c  VelocityX    0.70402E+08      17   0.15762E-01   0.58875E-02 
c  VelocityY    0.70402E+08      17   0.15762E-01   0.32867E-02 
c  VelocityZ    0.70402E+08      17   0.15762E-01   0.96529E-02 
c  TurbEner     0.95450E+07      29   0.27006E-04   0.31443E-03 
c  Dissip       0.39574E+07      16   0.29919E-04   0.41830E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -9.6464e-08                           123


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69340           71361          3809.1          6783.7
v  Velocity[x]            -6.9264          6.6902       -0.001243       0.0011237
v  Velocity[y]            -8.9859           7.254       -0.013042       -0.013185
v  Velocity[z]            -11.033          2.0098         -3.1513         -5.3361
v  TurbEner            0.00045832          9.1217         0.15904         0.27076
v  Dissip              7.4134e-12          5.3253        0.057744         0.10026
v  TurbVisc                1.1289      7.9079e+05          988.98          763.98
v  CourantNb                    0          2.7923         0.28158         0.45409
v  FourierNb           0.00068157          126.54         0.29843         0.20629
v  total_pressure           31985      1.7269e+05      1.0513e+05      1.0811e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013362          126.54         0.58001         0.66038


 TIME FOR THE TIME STEP               76:        0.19822E+00

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


 INSTANT    0.770000000E+01   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.170808451E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.86410E+01
   Friction velocity        uet   :  0.00000E+00 0.34112E+00
   Friction velocity        uk    :  0.11726E-01 0.60792E+00
   Dimensionless distance   yplus :  0.13244E+04 0.26549E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23110E+05     268   0.14301E-02   0.73665E-01 
c  VelocityX    0.70398E+08      17   0.16322E-01   0.57360E-02 
c  VelocityY    0.70398E+08      17   0.16322E-01   0.30750E-02 
c  VelocityZ    0.70398E+08      17   0.16322E-01   0.11211E-01 
c  TurbEner     0.95900E+07      18   0.26225E-04   0.30600E-03 
c  Dissip       0.39698E+07      28   0.28878E-04   0.41732E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -9.0421e-08                           141


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67524           70859          3843.7            6841
v  Velocity[x]            -6.8655           6.645       -0.001272       0.0010618
v  Velocity[y]            -8.9232          7.2305       -0.012776       -0.012776
v  Velocity[z]            -11.058          1.9999         -3.1512         -5.3361
v  TurbEner            0.00045681          9.1632         0.15945         0.27142
v  Dissip              3.3147e-11           5.345        0.057863         0.10044
v  TurbVisc                1.1272      4.5179e+06          1524.6          1161.5
v  CourantNb                    0          2.7905         0.28156         0.45407
v  FourierNb           0.00064995          453.95         0.40199         0.28443
v  total_pressure           33801      1.7218e+05      1.0517e+05      1.0817e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013347          453.95         0.68355          0.7385


 TIME FOR THE TIME STEP               77:        0.21743E+00

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


 INSTANT    0.780000000E+01   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.170869903E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.86219E+01
   Friction velocity        uet   :  0.00000E+00 0.34189E+00
   Friction velocity        uk    :  0.11707E-01 0.60205E+00
   Dimensionless distance   yplus :  0.13231E+04 0.26550E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23101E+05     283   0.14893E-02   0.73708E-01 
c  VelocityX    0.70395E+08      17   0.16958E-01   0.63360E-02 
c  VelocityY    0.70395E+08      17   0.16958E-01   0.46294E-02 
c  VelocityZ    0.70395E+08      17   0.16958E-01   0.91896E-02 
c  TurbEner     0.96336E+07      91   0.24350E-04   0.27965E-03 
c  Dissip       0.39807E+07      23   0.26839E-04   0.33624E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0379e-07                           131


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67617           71446          3831.7          6826.2
v  Velocity[x]            -6.8962          6.6806      -0.0013127       0.0009325
v  Velocity[y]            -8.8827          7.1823       -0.012888       -0.012954
v  Velocity[z]            -11.142          1.9879         -3.1513         -5.3362
v  TurbEner             0.0004553             9.2         0.15986         0.27206
v  Dissip              1.2595e-12          5.3607         0.05797          0.1006
v  TurbVisc                1.1256      1.0104e+06          1072.4          810.45
v  CourantNb                    0          2.7976         0.28155         0.45405
v  FourierNb           0.00065001          148.94         0.31306         0.21093
v  total_pressure           33708      1.7277e+05      1.0516e+05      1.0815e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013333          148.94          0.5946         0.66498


 TIME FOR THE TIME STEP               78:        0.21582E+00

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


 INSTANT    0.790000000E+01   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.347518714E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.86021E+01
   Friction velocity        uet   :  0.00000E+00 0.34586E+00
   Friction velocity        uk    :  0.11687E-01 0.59672E+00
   Dimensionless distance   yplus :  0.13218E+04 0.26547E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23526E+05     316   0.16189E-02   0.75298E-01 
c  VelocityX    0.70398E+08      18   0.17155E-01   0.61719E-02 
c  VelocityY    0.70398E+08      18   0.17155E-01   0.37014E-02 
c  VelocityZ    0.70398E+08      18   0.17155E-01   0.11013E-01 
c  TurbEner     0.96761E+07    3951   0.24382E-04   0.26554E-03 
c  Dissip       0.39911E+07    5812   0.27493E-04   0.32810E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.7033e-07                           121


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67204           71712          3956.1          7034.9
v  Velocity[x]            -6.8355          6.6587      -0.0014504      0.00073582
v  Velocity[y]            -8.9816          7.1532       -0.012827       -0.012871
v  Velocity[z]            -11.105          1.9804         -3.1514         -5.3365
v  TurbEner            0.00045381           9.234         0.16025         0.27269
v  Dissip              2.0181e-11          5.3746        0.058066         0.10074
v  TurbVisc                1.1239      2.6561e+07            8544          6171.4
v  CourantNb                    0          2.7924         0.28155         0.45404
v  FourierNb           0.00065006          3044.9          2.3292          1.5261
v  total_pressure           34121      1.7304e+05      1.0528e+05      1.0836e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013319          3044.9          2.6108          1.9801


 TIME FOR THE TIME STEP               79:        0.90182E+00

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


 INSTANT    0.800000000E+01   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.145625569E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.85782E+01
   Friction velocity        uet   :  0.00000E+00 0.34818E+00
   Friction velocity        uk    :  0.11668E-01 0.59188E+00
   Dimensionless distance   yplus :  0.13205E+04 0.26531E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23986E+05     300   0.14664E-02   0.76939E-01 
c  VelocityX    0.70403E+08      18   0.17053E-01   0.86427E-02 
c  VelocityY    0.70403E+08      18   0.17053E-01   0.34615E-02 
c  VelocityZ    0.70403E+08      18   0.17053E-01   0.10006E-01 
c  TurbEner     0.97186E+07      17   0.22996E-04   0.26509E-03 
c  Dissip       0.40024E+07      16   0.25962E-04   0.35270E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.2658e-07                           121


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67106           70924          3810.5          6783.9
v  Velocity[x]            -6.8002          6.6823       -0.001518      0.00067828
v  Velocity[y]              -8.92          7.1312       -0.012757       -0.012733
v  Velocity[z]            -11.059          1.9708         -3.1512         -5.3363
v  TurbEner            0.00045232          9.2671         0.16067         0.27334
v  Dissip              3.1019e-11          5.3884        0.058183         0.10091
v  TurbVisc                1.1223      1.6586e+06          1036.8          788.12
v  CourantNb                    0           2.799         0.28154         0.45404
v  FourierNb           0.00065019          188.03         0.30829         0.20564
v  total_pressure           34219      1.7225e+05      1.0514e+05      1.0811e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013305          188.03         0.58982         0.65968


 TIME FOR THE TIME STEP               80:        0.20804E+00

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


 INSTANT    0.810000000E+01   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.214210651E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.85558E+01
   Friction velocity        uet   :  0.00000E+00 0.35106E+00
   Friction velocity        uk    :  0.11649E-01 0.58757E+00
   Dimensionless distance   yplus :  0.13192E+04 0.26513E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23619E+05     269   0.14530E-02   0.75523E-01 
c  VelocityX    0.70391E+08      17   0.17486E-01   0.70956E-02 
c  VelocityY    0.70391E+08      17   0.17486E-01   0.32311E-02 
c  VelocityZ    0.70391E+08      17   0.17486E-01   0.79708E-02 
c  TurbEner     0.97603E+07      19   0.22413E-04   0.25207E-03 
c  Dissip       0.40134E+07      16   0.26657E-04   0.33586E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip         -7.23e-08                           131


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -65852           70936          3834.6          6825.4
v  Velocity[x]            -6.8745          6.6521      -0.0015848      0.00043389
v  Velocity[y]            -8.8246           7.201       -0.012514       -0.012392
v  Velocity[z]            -11.062          1.9615         -3.1512         -5.3362
v  TurbEner            0.00045084          9.2988         0.16109         0.27399
v  Dissip              4.0184e-11          5.4013        0.058298         0.10108
v  TurbVisc                1.1207      1.0802e+06          1267.4          963.59
v  CourantNb                    0          2.7952         0.28153         0.45402
v  FourierNb           0.00065035          121.72         0.36489         0.24663
v  total_pressure           35473      1.7226e+05      1.0516e+05      1.0815e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013291          121.72         0.64642         0.70065


 TIME FOR THE TIME STEP               81:        0.20705E+00

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


 INSTANT    0.820000000E+01   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.959124600E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393705E+07
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 0.85373E+01
   Friction velocity        uet   :  0.00000E+00 0.35235E+00
   Friction velocity        uk    :  0.11630E-01 0.58382E+00
   Dimensionless distance   yplus :  0.13179E+04 0.26491E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24970E+05     290   0.17896E-02   0.79913E-01 
c  VelocityX    0.70397E+08      17   0.16163E-01   0.71809E-02 
c  VelocityY    0.70397E+08      17   0.16163E-01   0.39048E-02 
c  VelocityZ    0.70397E+08      17   0.16163E-01   0.13456E-01 
c  TurbEner     0.98009E+07     138   0.21107E-04   0.24056E-03 
c  Dissip       0.40241E+07     136   0.24299E-04   0.32769E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.4835e-07                           124


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68194           71668          3980.7            7076
v  Velocity[x]            -6.9171          6.6736      -0.0018123      0.00027702
v  Velocity[y]            -8.8174          7.1705        -0.01234       -0.012201
v  Velocity[z]            -11.059          1.9541         -3.1513         -5.3366
v  TurbEner            0.00044937          9.3297         0.16151         0.27462
v  Dissip               1.096e-12          5.4139        0.058411         0.10124
v  TurbVisc                1.1192      8.3144e+05          1040.7          840.69
v  CourantNb                    0           2.798         0.28152           0.454
v  FourierNb           0.00065029          100.95         0.31277         0.22104
v  total_pressure           33131      1.7299e+05      1.0531e+05       1.084e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013278          100.95         0.59429         0.67504


 TIME FOR THE TIME STEP               82:        0.24234E+00

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


 INSTANT    0.830000000E+01   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.213261617E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.85169E+01
   Friction velocity        uet   :  0.00000E+00 0.35307E+00
   Friction velocity        uk    :  0.11611E-01 0.58169E+00
   Dimensionless distance   yplus :  0.13167E+04 0.26468E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24040E+05     276   0.15454E-02   0.76468E-01 
c  VelocityX    0.70403E+08      17   0.16483E-01   0.52347E-02 
c  VelocityY    0.70403E+08      17   0.16483E-01   0.42017E-02 
c  VelocityZ    0.70403E+08      17   0.16483E-01   0.95645E-02 
c  TurbEner     0.98407E+07    7657   0.20929E-04   0.22698E-03 
c  Dissip       0.40343E+07      51   0.22869E-04   0.28155E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -5.4602e-08                           126


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68785           71160          3839.4          6840.6
v  Velocity[x]            -6.8854          6.6798      -0.0018542      0.00011384
v  Velocity[y]            -8.8141          7.1547       -0.012312       -0.012278
v  Velocity[z]            -11.062          1.9495         -3.1515         -5.3368
v  TurbEner             0.0004479          9.3615         0.16192         0.27525
v  Dissip              8.5064e-12          5.4277        0.058516          0.1014
v  TurbVisc                1.1176      3.0511e+07            5111          4329.9
v  CourantNb                    0          2.7947         0.28152         0.45399
v  FourierNb           0.00065032            5019          1.7164          1.3355
v  total_pressure           32540      1.7249e+05      1.0516e+05      1.0817e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013264            5019           1.998          1.7894


 TIME FOR THE TIME STEP               83:        0.78311E+00

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


 INSTANT    0.840000000E+01   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.306077300E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393703E+07
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 0.84951E+01
   Friction velocity        uet   :  0.00000E+00 0.35414E+00
   Friction velocity        uk    :  0.11592E-01 0.58134E+00
   Dimensionless distance   yplus :  0.13154E+04 0.26450E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23415E+05     295   0.14692E-02   0.74870E-01 
c  VelocityX    0.70399E+08      18   0.16521E-01   0.74848E-02 
c  VelocityY    0.70399E+08      18   0.16521E-01   0.32702E-02 
c  VelocityZ    0.70399E+08      18   0.16521E-01   0.92339E-02 
c  TurbEner     0.98805E+07     188   0.20156E-04   0.22731E-03 
c  Dissip       0.40451E+07     409   0.23146E-04   0.29512E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -3.0404e-07                           129


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68178           70301          3757.2          6698.3
v  Velocity[x]             -6.856          6.6708      -0.0020218     -3.1496e-05
v  Velocity[y]            -8.8599          7.1409       -0.012419       -0.012486
v  Velocity[z]            -11.079          1.9415         -3.1514         -5.3366
v  TurbEner            0.00044644          9.3914         0.16236         0.27591
v  Dissip              2.5205e-11          5.4398        0.058634         0.10157
v  TurbVisc                1.1161      3.9202e+06          1461.3          1498.3
v  CourantNb                    0          2.7926         0.28152         0.45398
v  FourierNb           0.00065033          371.88         0.40944         0.34355
v  total_pressure           33147      1.7163e+05      1.0508e+05      1.0802e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013251          371.88         0.69096         0.79754


 TIME FOR THE TIME STEP               84:        0.25430E+00

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


 INSTANT    0.850000000E+01   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.197179299E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.84778E+01
   Friction velocity        uet   :  0.00000E+00 0.35384E+00
   Friction velocity        uk    :  0.11573E-01 0.58103E+00
   Dimensionless distance   yplus :  0.13141E+04 0.26432E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22735E+05     308   0.14721E-02   0.72545E-01 
c  VelocityX    0.70391E+08      18   0.19382E-01   0.60954E-02 
c  VelocityY    0.70391E+08      18   0.19382E-01   0.41212E-02 
c  VelocityZ    0.70391E+08      18   0.19382E-01   0.10326E-01 
c  TurbEner     0.99187E+07     204   0.19387E-04   0.20600E-03 
c  Dissip       0.40546E+07      82   0.21563E-04   0.22878E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.2664e-07                           120


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68634           70859          3899.1          6933.6
v  Velocity[x]            -6.9872          6.6665      -0.0021262      -9.485e-05
v  Velocity[y]            -8.9197          7.1194       -0.012571       -0.012835
v  Velocity[z]              -11.1          1.9382         -3.1514         -5.3366
v  TurbEner            0.00044499          9.4216         0.16277         0.27654
v  Dissip              3.7876e-11          5.4524        0.058737         0.10172
v  TurbVisc                1.1146      1.3249e+06          1169.7          906.69
v  CourantNb                    0          2.7968         0.28152         0.45398
v  FourierNb           0.00065031          268.71         0.41305         0.25288
v  total_pressure           32691      1.7218e+05      1.0522e+05      1.0826e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013237          268.71         0.69457         0.70686


 TIME FOR THE TIME STEP               85:        0.21632E+00

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


 INSTANT    0.860000000E+01   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.199194147E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.84651E+01
   Friction velocity        uet   :  0.00000E+00 0.35492E+00
   Friction velocity        uk    :  0.11554E-01 0.58057E+00
   Dimensionless distance   yplus :  0.13129E+04 0.26430E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27513E+05     259   0.17589E-02   0.87805E-01 
c  VelocityX    0.70383E+08      17   0.17693E-01   0.71105E-02 
c  VelocityY    0.70383E+08      17   0.17693E-01   0.42005E-02 
c  VelocityZ    0.70383E+08      17   0.17693E-01   0.16088E-01 
c  TurbEner     0.99569E+07      17   0.18341E-04   0.20864E-03 
c  Dissip       0.40643E+07      16   0.20645E-04   0.24058E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0193e-07                           111


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66736           72152          3913.2          6963.6
v  Velocity[x]            -6.9449          6.6987       -0.002053     -0.00011696
v  Velocity[y]            -8.8802          7.2132       -0.012537       -0.012794
v  Velocity[z]            -11.036          1.9337         -3.1517         -5.3372
v  TurbEner            0.00044355          9.4533          0.1632          0.2772
v  Dissip              1.3807e-11          5.4661        0.058852         0.10189
v  TurbVisc                1.1131      8.8333e+05          1018.6          771.15
v  CourantNb                    0          2.7942         0.28152         0.45397
v  FourierNb           0.00065047          100.81         0.30754         0.20685
v  total_pressure           34589      1.7348e+05      1.0524e+05      1.0829e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013224          100.81         0.58907         0.66082


 TIME FOR THE TIME STEP               86:        0.21516E+00

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


 INSTANT    0.870000000E+01   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.453351794E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393704E+07
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 0.84649E+01
   Friction velocity        uet   :  0.00000E+00 0.34230E+00
   Friction velocity        uk    :  0.11535E-01 0.57999E+00
   Dimensionless distance   yplus :  0.13117E+04 0.26428E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25181E+05     299   0.16042E-02   0.80134E-01 
c  VelocityX    0.70413E+08      17   0.17439E-01   0.64503E-02 
c  VelocityY    0.70413E+08      17   0.17439E-01   0.29038E-02 
c  VelocityZ    0.70413E+08      17   0.17439E-01   0.11966E-01 
c  TurbEner     0.99953E+07      90   0.19784E-04   0.20564E-03 
c  Dissip       0.40745E+07      24   0.22804E-04   0.23568E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -5.5795e-07                           119


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68286           70636          3745.7            6679
v  Velocity[x]            -6.8712          6.6867      -0.0021883     -0.00012912
v  Velocity[y]            -8.8608           7.151       -0.012675       -0.013078
v  Velocity[z]            -11.059          1.9311         -3.1517         -5.3373
v  TurbEner            0.00044212          9.4867         0.16364         0.27787
v  Dissip              6.1645e-12          5.4816        0.058973         0.10207
v  TurbVisc                1.1116      2.4223e+06          1303.6          1045.6
v  CourantNb                    0             2.8         0.28153         0.45397
v  FourierNb           0.00065152           343.6         0.40262         0.28543
v  total_pressure           33039      1.7196e+05      1.0507e+05        1.08e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013211           343.6         0.68414          0.7394


 TIME FOR THE TIME STEP               87:        0.24411E+00

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


 INSTANT    0.880000000E+01   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.388258705E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.84688E+01
   Friction velocity        uet   :  0.00000E+00 0.34310E+00
   Friction velocity        uk    :  0.11517E-01 0.57985E+00
   Dimensionless distance   yplus :  0.13104E+04 0.26427E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25214E+05     274   0.15299E-02   0.80264E-01 
c  VelocityX    0.70397E+08      18   0.16660E-01   0.86609E-02 
c  VelocityY    0.70397E+08      18   0.16660E-01   0.32336E-02 
c  VelocityZ    0.70397E+08      18   0.16660E-01   0.10608E-01 
c  TurbEner     0.10033E+08     631   0.18361E-04   0.19961E-03 
c  Dissip       0.40840E+07     207   0.20381E-04   0.22732E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.0454e-07                           114


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69588           71072          3790.3          6750.8
v  Velocity[x]            -6.9575          6.7372      -0.0021817     -3.6429e-05
v  Velocity[y]            -8.9489          7.1332       -0.012798       -0.013403
v  Velocity[z]            -11.046          1.9326         -3.1517         -5.3374
v  TurbEner            0.00044069          9.5166         0.16408         0.27855
v  Dissip              2.8705e-11          5.4942        0.059089         0.10225
v  TurbVisc                1.1101      5.4085e+06          1988.4          1749.1
v  CourantNb                    0          2.7937         0.28153         0.45397
v  FourierNb           0.00065042          622.17         0.57598         0.43465
v  total_pressure           31737       1.724e+05      1.0512e+05      1.0808e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013199          622.17         0.85751         0.88862


 TIME FOR THE TIME STEP               88:        0.26122E+00

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


 INSTANT    0.890000000E+01   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.686611359E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.84737E+01
   Friction velocity        uet   :  0.00000E+00 0.34288E+00
   Friction velocity        uk    :  0.11498E-01 0.58014E+00
   Dimensionless distance   yplus :  0.13092E+04 0.26428E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24041E+05     274   0.13642E-02   0.76464E-01 
c  VelocityX    0.70407E+08      18   0.15023E-01   0.79642E-02 
c  VelocityY    0.70407E+08      18   0.15023E-01   0.35963E-02 
c  VelocityZ    0.70407E+08      18   0.15023E-01   0.83105E-02 
c  TurbEner     0.10071E+08      52   0.20002E-04   0.20328E-03 
c  Dissip       0.40940E+07     172   0.24369E-04   0.24490E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -2.7107e-07                            92


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69515           70483          3823.4          6805.2
v  Velocity[x]            -6.9203          6.7053      -0.0021099      6.6949e-05
v  Velocity[y]            -8.9385          7.0996       -0.012851       -0.013625
v  Velocity[z]            -11.067          1.9298         -3.1516         -5.3374
v  TurbEner            0.00043927          9.5452         0.16453         0.27924
v  Dissip              1.7506e-11           5.506         0.05921         0.10243
v  TurbVisc                1.1087      1.1676e+06          1240.3          1032.5
v  CourantNb                    0          2.7989         0.28151         0.45395
v  FourierNb           0.00065034          145.99         0.37744         0.27093
v  total_pressure           31810      1.7181e+05      1.0515e+05      1.0813e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013186          145.99         0.65895         0.72488


 TIME FOR THE TIME STEP               89:        0.21371E+00

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


 INSTANT    0.900000000E+01   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.104390026E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.84744E+01
   Friction velocity        uet   :  0.00000E+00 0.34266E+00
   Friction velocity        uk    :  0.11480E-01 0.58101E+00
   Dimensionless distance   yplus :  0.13080E+04 0.26434E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22086E+05     297   0.13517E-02   0.70018E-01 
c  VelocityX    0.70410E+08      17   0.16799E-01   0.40102E-02 
c  VelocityY    0.70410E+08      17   0.16799E-01   0.34149E-02 
c  VelocityZ    0.70410E+08      17   0.16799E-01   0.87648E-02 
c  TurbEner     0.10110E+08     228   0.19950E-04   0.20437E-03 
c  Dissip       0.41043E+07     375   0.22827E-04   0.24491E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -4.4682e-08                           102


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69474           70684          3726.3          6641.4
v  Velocity[x]            -6.9875          6.7449      -0.0020585      0.00018003
v  Velocity[y]            -8.9101          7.0538       -0.012998       -0.013955
v  Velocity[z]            -11.093           1.928         -3.1516         -5.3374
v  TurbEner            0.00043786          9.5707         0.16499         0.27996
v  Dissip              3.3101e-12          5.5147        0.059335         0.10263
v  TurbVisc                1.1072      1.9028e+06          1133.7          939.63
v  CourantNb                    0          2.7951          0.2815         0.45394
v  FourierNb           0.00065028          268.48         0.34967         0.24844
v  total_pressure           31851      1.7201e+05      1.0505e+05      1.0797e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013174          268.48         0.63117         0.70238


 TIME FOR THE TIME STEP               90:        0.25402E+00

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


 INSTANT    0.910000000E+01   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.176628096E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393700E+07
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 0.84742E+01
   Friction velocity        uet   :  0.00000E+00 0.34589E+00
   Friction velocity        uk    :  0.11461E-01 0.58239E+00
   Dimensionless distance   yplus :  0.13068E+04 0.26439E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25955E+05     297   0.15924E-02   0.82568E-01 
c  VelocityX    0.70403E+08      18   0.17149E-01   0.75452E-02 
c  VelocityY    0.70403E+08      18   0.17149E-01   0.36314E-02 
c  VelocityZ    0.70403E+08      18   0.17149E-01   0.11121E-01 
c  TurbEner     0.10149E+08    3352   0.19613E-04   0.20645E-03 
c  Dissip       0.41153E+07    2779   0.27018E-04   0.27203E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -8.1055e-08                           127


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69878           71169          3883.2          6904.8
v  Velocity[x]            -6.9616          6.7109      -0.0019425      0.00026438
v  Velocity[y]            -8.9621          7.1293       -0.013051       -0.014088
v  Velocity[z]            -11.136          1.9275         -3.1517         -5.3376
v  TurbEner            0.00043646           9.594         0.16546          0.2807
v  Dissip              3.8689e-11          5.5211        0.059469         0.10284
v  TurbVisc                1.1058      1.0093e+07          3394.1          2500.8
v  CourantNb                    0          2.7973          0.2815         0.45393
v  FourierNb           0.00065029          1815.7          1.0469         0.71355
v  total_pressure           31447      1.7249e+05      1.0521e+05      1.0823e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013162          1815.7          1.3284          1.1675


 TIME FOR THE TIME STEP               91:        0.62836E+00

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


 INSTANT    0.920000000E+01   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.201392999E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393707E+07
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 0.84794E+01
   Friction velocity        uet   :  0.00000E+00 0.34921E+00
   Friction velocity        uk    :  0.11443E-01 0.58420E+00
   Dimensionless distance   yplus :  0.13056E+04 0.26455E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24301E+05     236   0.14921E-02   0.77335E-01 
c  VelocityX    0.70414E+08      18   0.16513E-01   0.61493E-02 
c  VelocityY    0.70414E+08      18   0.16513E-01   0.35973E-02 
c  VelocityZ    0.70414E+08      18   0.16513E-01   0.11291E-01 
c  TurbEner     0.10189E+08      45   0.19256E-04   0.20785E-03 
c  Dissip       0.41265E+07      17   0.24146E-04   0.26019E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -7.2175e-08                           106


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69955           70955          3901.6          6937.3
v  Velocity[x]            -6.9185          6.6923      -0.0018651      0.00047443
v  Velocity[y]            -8.9255          7.1237       -0.013238         -0.0145
v  Velocity[z]            -11.081          1.9227         -3.1519         -5.3381
v  TurbEner            0.00043506          9.6116         0.16593         0.28145
v  Dissip              5.5332e-11          5.5221        0.059607         0.10306
v  TurbVisc                1.1044      8.6357e+05          910.61          726.46
v  CourantNb                    0          2.7932         0.28147         0.45389
v  FourierNb           0.00065033          124.65         0.28121         0.19667
v  total_pressure           31370      1.7228e+05      1.0523e+05      1.0826e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001315          124.65         0.56268         0.65056


 TIME FOR THE TIME STEP               92:        0.21514E+00

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


 INSTANT    0.930000000E+01   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.418771646E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.84795E+01
   Friction velocity        uet   :  0.00000E+00 0.35092E+00
   Friction velocity        uk    :  0.11424E-01 0.58645E+00
   Dimensionless distance   yplus :  0.13044E+04 0.26470E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23602E+05     292   0.16026E-02   0.74926E-01 
c  VelocityX    0.70426E+08      17   0.15931E-01   0.59489E-02 
c  VelocityY    0.70426E+08      17   0.15931E-01   0.34710E-02 
c  VelocityZ    0.70426E+08      17   0.15931E-01   0.93425E-02 
c  TurbEner     0.10229E+08      16   0.20327E-04   0.20630E-03 
c  Dissip       0.41375E+07      60   0.26440E-04   0.27866E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -9.3647e-08                            97


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69929           69799          3744.7            6675
v  Velocity[x]              -7.05          6.6843      -0.0018838      0.00048918
v  Velocity[y]            -8.8748           7.114       -0.013471       -0.014938
v  Velocity[z]            -11.108          1.9229         -3.1518         -5.3381
v  TurbEner            0.00043367          9.6225          0.1664         0.28219
v  Dissip              9.0192e-11          5.5174        0.059734         0.10327
v  TurbVisc                 1.103      6.0235e+05          928.15          765.26
v  CourantNb                    0          2.7985         0.28149         0.45392
v  FourierNb           0.00065045          76.746         0.27981          0.1998
v  total_pressure           31396      1.7112e+05      1.0507e+05        1.08e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013138          76.746          0.5613         0.65372


 TIME FOR THE TIME STEP               93:        0.21382E+00

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


 INSTANT    0.940000000E+01   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.199156337E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.84845E+01
   Friction velocity        uet   :  0.00000E+00 0.35199E+00
   Friction velocity        uk    :  0.11406E-01 0.58895E+00
   Dimensionless distance   yplus :  0.13033E+04 0.26491E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24228E+05     272   0.17090E-02   0.76634E-01 
c  VelocityX    0.70422E+08      17   0.18083E-01   0.73091E-02 
c  VelocityY    0.70422E+08      17   0.18083E-01   0.33852E-02 
c  VelocityZ    0.70422E+08      17   0.18083E-01   0.10329E-01 
c  TurbEner     0.10270E+08      35   0.21465E-04   0.21459E-03 
c  Dissip       0.41501E+07      18   0.27106E-04   0.29092E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -1.057e-07                           104


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -70307           71724          3851.9          6856.4
v  Velocity[x]            -7.0141          6.7358      -0.0016142      0.00090932
v  Velocity[y]            -8.8313          7.0902       -0.013438       -0.015031
v  Velocity[z]            -11.079           1.921         -3.1522         -5.3385
v  TurbEner            0.00043229          9.6436         0.16689         0.28298
v  Dissip              8.0878e-12          5.5214        0.059882         0.10351
v  TurbVisc                1.1016      3.7102e+05          944.19          755.45
v  CourantNb                    0          2.7937         0.28147          0.4539
v  FourierNb           0.00065054          54.225          0.2867         0.19872
v  total_pressure           31018      1.7305e+05      1.0518e+05      1.0818e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013127          54.225         0.56817         0.65261


 TIME FOR THE TIME STEP               94:        0.20197E+00

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


 INSTANT    0.950000000E+01   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.886943090E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393701E+07
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 0.84850E+01
   Friction velocity        uet   :  0.00000E+00 0.35292E+00
   Friction velocity        uk    :  0.11388E-01 0.59175E+00
   Dimensionless distance   yplus :  0.13021E+04 0.26517E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25256E+05     254   0.14728E-02   0.80114E-01 
c  VelocityX    0.70428E+08      18   0.17816E-01   0.99318E-02 
c  VelocityY    0.70428E+08      18   0.17816E-01   0.52639E-02 
c  VelocityZ    0.70428E+08      18   0.17816E-01   0.93645E-02 
c  TurbEner     0.10311E+08     171   0.20169E-04   0.20409E-03 
c  Dissip       0.41619E+07      55   0.24854E-04   0.27103E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip        -9.741e-08                           103


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69841           70849          3848.3          6843.5
v  Velocity[x]            -6.9097          6.7038      -0.0013679       0.0011433
v  Velocity[y]            -8.9429          7.1497       -0.013519       -0.015073
v  Velocity[z]            -11.023          1.9156         -3.1522         -5.3386
v  TurbEner            0.00043092          9.6637         0.16736         0.28374
v  Dissip              4.0995e-11          5.5244        0.060017         0.10374
v  TurbVisc                1.1003      4.1315e+06          1420.2          1030.9
v  CourantNb                    0          2.7978         0.28147         0.45388
v  FourierNb           0.00065057          479.95         0.38663         0.25941
v  total_pressure           31484      1.7217e+05      1.0517e+05      1.0817e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013114          479.95         0.66809         0.71329


 TIME FOR THE TIME STEP               95:        0.22554E+00

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


 INSTANT    0.960000000E+01   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.367806643E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393704E+07
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 0.84939E+01
   Friction velocity        uet   :  0.00000E+00 0.35406E+00
   Friction velocity        uk    :  0.11370E-01 0.59472E+00
   Dimensionless distance   yplus :  0.13009E+04 0.26552E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24223E+05     272   0.13968E-02   0.76560E-01 
c  VelocityX    0.70427E+08      17   0.15924E-01   0.72142E-02 
c  VelocityY    0.70427E+08      17   0.15924E-01   0.30451E-02 
c  VelocityZ    0.70427E+08      17   0.15924E-01   0.10322E-01 
c  TurbEner     0.10353E+08      44   0.22073E-04   0.21793E-03 
c  Dissip       0.41752E+07      85   0.26398E-04   0.29789E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -6.2177e-08                           120


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -69355           71573          3771.7            6720
v  Velocity[x]            -6.9653          6.7517      -0.0011544       0.0014845
v  Velocity[y]            -8.9204          7.1637       -0.013732       -0.015457
v  Velocity[z]            -11.048          1.9143         -3.1523         -5.3387
v  TurbEner            0.00042955          9.6878         0.16786         0.28453
v  Dissip              5.2923e-11          5.5309        0.060172         0.10399
v  TurbVisc                1.0989      8.1593e+05          1199.1          960.72
v  CourantNb                    0          2.7961         0.28145         0.45387
v  FourierNb           0.00065067           131.8         0.37773         0.25913
v  total_pressure           31970       1.729e+05       1.051e+05      1.0805e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013103           131.8         0.65918           0.713


 TIME FOR THE TIME STEP               96:        0.22548E+00

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


 INSTANT    0.970000000E+01   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.834487171E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393703E+07
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 0.84998E+01
   Friction velocity        uet   :  0.00000E+00 0.35504E+00
   Friction velocity        uk    :  0.11352E-01 0.59788E+00
   Dimensionless distance   yplus :  0.12998E+04 0.26589E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24614E+05     291   0.16047E-02   0.77891E-01 
c  VelocityX    0.70422E+08      17   0.19660E-01   0.62122E-02 
c  VelocityY    0.70422E+08      17   0.19660E-01   0.39877E-02 
c  VelocityZ    0.70422E+08      17   0.19660E-01   0.99924E-02 
c  TurbEner     0.10394E+08      16   0.19790E-04   0.20981E-03 
c  Dissip       0.41881E+07      15   0.26631E-04   0.28919E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.6811e-07                            94


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68304           71260          3880.6          6902.4
v  Velocity[x]             -6.895          6.7109      -0.0011261       0.0014331
v  Velocity[y]            -8.9008          7.1343       -0.013978       -0.015877
v  Velocity[z]            -11.096          1.9101         -3.1523         -5.3388
v  TurbEner            0.00042819          9.7171         0.16833         0.28531
v  Dissip               5.133e-11          5.5419        0.060317         0.10423
v  TurbVisc                1.0976      6.3231e+05          816.39          606.49
v  CourantNb                    0          2.7979         0.28143         0.45385
v  FourierNb           0.00065053           94.27         0.24417         0.16219
v  total_pressure           33021      1.7258e+05      1.0521e+05      1.0823e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013092           94.27         0.52561         0.61604


 TIME FOR THE TIME STEP               97:        0.20829E+00

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


 INSTANT    0.980000000E+01   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.614488956E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.85041E+01
   Friction velocity        uet   :  0.00000E+00 0.35518E+00
   Friction velocity        uk    :  0.11334E-01 0.60102E+00
   Dimensionless distance   yplus :  0.12986E+04 0.26655E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26341E+05     264   0.18268E-02   0.83565E-01 
c  VelocityX    0.70424E+08      17   0.19486E-01   0.64890E-02 
c  VelocityY    0.70424E+08      17   0.19486E-01   0.33152E-02 
c  VelocityZ    0.70424E+08      17   0.19486E-01   0.16421E-01 
c  TurbEner     0.10435E+08      16   0.18885E-04   0.21343E-03 
c  Dissip       0.42016E+07      20   0.21477E-04   0.28193E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -6.3147e-08                           111


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -66583           71531          3902.9            6938
v  Velocity[x]            -6.8774          6.6682     -0.00094987        0.001771
v  Velocity[y]            -8.8668          7.2268       -0.013794       -0.015677
v  Velocity[z]            -11.141           1.906         -3.1526         -5.3394
v  TurbEner            0.00042683          9.7519         0.16883          0.2861
v  Dissip              1.9819e-11           5.557        0.060472         0.10449
v  TurbVisc                1.0963      6.5087e+05          926.81          776.94
v  CourantNb                    0          2.7958         0.28143         0.45386
v  FourierNb              0.00065          75.208         0.28301         0.20186
v  total_pressure           34742      1.7286e+05      1.0523e+05      1.0826e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013081          75.208         0.56444         0.65572


 TIME FOR THE TIME STEP               98:        0.19955E+00

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


 INSTANT    0.990000000E+01   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832         0.227967646E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393702E+07
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 0.85068E+01
   Friction velocity        uet   :  0.00000E+00 0.34298E+00
   Friction velocity        uk    :  0.11316E-01 0.60425E+00
   Dimensionless distance   yplus :  0.12975E+04 0.26798E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26511E+05     275   0.17846E-02   0.84282E-01 
c  VelocityX    0.70435E+08      18   0.17249E-01   0.82079E-02 
c  VelocityY    0.70435E+08      18   0.17249E-01   0.33987E-02 
c  VelocityZ    0.70435E+08      18   0.17249E-01   0.11359E-01 
c  TurbEner     0.10478E+08      81   0.20156E-04   0.21374E-03 
c  Dissip       0.42153E+07     163   0.23077E-04   0.28352E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -7.5783e-08                           110


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -67349           71098          3790.2          6754.3
v  Velocity[x]            -6.9435          6.6805     -0.00081119       0.0020295
v  Velocity[y]            -8.8702          7.1677       -0.013955       -0.015918
v  Velocity[z]            -11.088          1.9188         -3.1527         -5.3396
v  TurbEner            0.00042549          9.7887         0.16931         0.28689
v  Dissip              1.4541e-11          5.5736        0.060624         0.10474
v  TurbVisc                 1.095       1.687e+06            1246            1065
v  CourantNb                    0          2.7996         0.28144         0.45385
v  FourierNb           0.00065053          239.27         0.36602         0.27222
v  total_pressure           33976      1.7242e+05      1.0512e+05      1.0808e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001307          239.27         0.64746         0.72607


 TIME FOR THE TIME STEP               99:        0.21354E+00

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          52        -0.358393704E+07
Smooth wall               5        1832        -0.982369447E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4        2052         0.000000000E+00
Free outlet               3          48         0.358393706E+07
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 0.85182E+01
   Friction velocity        uet   :  0.00000E+00 0.34291E+00
   Friction velocity        uk    :  0.11298E-01 0.60735E+00
   Dimensionless distance   yplus :  0.12964E+04 0.26935E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1832
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         48
 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.4058e-01; norm:  6.4477e-12


 Write final restart files
   checkpoint at iteration        100, Physical time    0.10000E+02


   ** 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:    0.48506E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24453E+05     297   0.14973E-02   0.78008E-01 
c  VelocityX    0.70430E+08      17   0.15336E-01   0.61298E-02 
c  VelocityY    0.70430E+08      17   0.15336E-01   0.34980E-02 
c  VelocityZ    0.70430E+08      17   0.15336E-01   0.97825E-02 
c  TurbEner     0.10519E+08      16   0.19471E-04   0.20927E-03 
c  Dissip       0.42284E+07     797   0.22623E-04   0.27706E-04 
---------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip       -1.3967e-07                           112


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -68641           70879            3748          6681.4
v  Velocity[x]            -6.9526          6.6811     -0.00075432       0.0021451
v  Velocity[y]            -8.8975          7.1213       -0.014158       -0.016331
v  Velocity[z]            -11.108          1.9265         -3.1525         -5.3394
v  TurbEner            0.00042415          9.8247         0.16979         0.28767
v  Dissip              7.7969e-11          5.5895        0.060771         0.10499
v  TurbVisc                1.0937      2.2947e+06          1027.9           799.1
v  CourantNb                    0          2.7961         0.28144         0.45385
v  FourierNb            0.0006501          446.73          0.3579         0.23824
v  total_pressure           32684       1.722e+05      1.0507e+05      1.0801e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013059          446.73         0.63934         0.69209


 TIME FOR THE TIME STEP              100:        0.26985E+00

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.24333E-03
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:             30.748 s
  System CPU time:            3.836 s

  Elapsed time:              35.142 s
  CPU / elapsed time          0.984

Memory use summary:

  Total memory used:                             102.824 MiB
  Theoretical instrumented dynamic memory:         6.555 MiB
