command: 
 /opt/code_saturne-3.2.1/arch/Linux_x86_64/libexec/code_saturne/cs_solver --param PorousMediaTestCase.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.2.1


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

  build Fri 14 Mar 2014 03:31:14 PM CET
  MPI version 2.1 (Open MPI 1.4.5)


  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:                Mon 30 Mar 2015 12:50:00 PM CEST
  System:              Linux 3.8.0-35-generic
  Machine:             Ren-FR-WS3
  Processor:           model name	: Intel(R) Xeon(R) CPU           X5650  @ 2.67GHz
  Memory:              48297 MB
  User:                brianangel (brianangel)
  Directory:           /home/brianangel/PROJECTS/CONSULTING/EDF/CHATOU/2015_STUDIES/SUPPORT/POROUS_MEDIA/POR_MEDIA/TEST_CASE/RESU/20150330-1249
  MPI ranks:           4 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    ParMETIS 4.0.3
    PT-SCOTCH 6.0.0

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

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

                   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     =   -0.98100E+01 (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    =    0.10000E+04 (Reference density           )
       VISCL0 =    0.10000E-02 (Ref. molecular dyn. visc.   )
       CP0    =    0.41830E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10133E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             21 (Turbulence model            )
       IDEUCH =              1 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - Linear production k-epsilon (ITURB = 21)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              0 (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))

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


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


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

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


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


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

    STEADY ALGORITHM

 --- Global parameters

       IDTVAR =             -1 (-1: steady algorithm        )
       RELXST =    0.70000E+00 (Reference relaxation coeff. )


 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per variable relaxation coefficient

-----------------------------
 Variable          RELAXV
-----------------------------
 Pressure          0.3000E+00
 VelocityX         0.7000E+00
 VelocityY         0.7000E+00
 VelocityZ         0.7000E+00
 TurbEner          0.7000E+00
 Dissip            0.7000E+00
----------------------------

       RELAXV =  [0.,1.]       (relaxation coefficient      )


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


 ** 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)

       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 =              3 (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-03  0.0000E+00
 VelocityX           100      1  0.1000E-04  0.1000E-03  0.0000E+00
 VelocityY           100      1  0.1000E-04  0.1000E-03  0.0000E+00
 VelocityZ           100      1  0.1000E-04  0.1000E-03  0.0000E+00
 TurbEner            100      1  0.1000E-04  0.1000E-03  0.0000E+00
 Dissip              100      1  0.1000E-04  0.1000E-03  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-04      1
 VelocityX            -1  10000  0.1000E-04      1
 VelocityY            -1  10000  0.1000E-04      1
 VelocityZ            -1  10000  0.1000E-04      1
 TurbEner             -1  10000  0.1000E-04      1
 Dissip               -1  10000  0.1000E-04      1
-----------------------------------

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


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


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

       NCEGRM =             30 (Max nb cells coarsest grid  )
       NGRMAX =             25 (Max number of levels        )
--------------------------------------
 Variable           IMGR NCYMAX NITMGF
--------------------------------------                       
 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 rank merge parameters:
    mean  coarse cells merge threshold: 300
    total coarse cells merge threshold: 500
    minimum ranks merge threshold:      1
    merge stride:                       1

  Multigrid coarsening type: algebraic, face traveral by criteria

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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =           1000 (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        
        13 total_pressure  
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              5 (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
        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
        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: every 500 time steps and at calculation end


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

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

 Reading file:        mesh_input/mesh_03
 Finished reading:    mesh_input/mesh_03
 No "partition_input/domain_number_4" file available;

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [       5579 ;       5580 ] =          4

 Partitioning finished (0.0851 s)


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

  Selection criteria: "Interface_1"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.10000
    Maximum angle between joined face planes: 25.00000

  Advanced joining parameters:
    Verbosity level:                                 1
    Visualization level:                             1
    Deepest level reachable in tree building:       30
    Max boxes by leaf:                              25
    Max ratio of linked boxes / init. boxes:   5.00000
    Max ratio of boxes for distribution:       2.00000
    Merge step tolerance multiplier:           1.00000
    Pre-merge factor:                          0.05000
    Tolerance computation mode:                      1
    Intersection computation mode:                   1
    Max. number of equiv. breaks:                  500
    Max. number of subfaces by face:               200

  Before joining
     Number of cells:          22319
     Number of interior faces: 43828
     Number of boundary faces: 4390
     Number of vertices:       5933

  Global number of boundary faces selected for joining:        540

  Element selection successfully done.
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

         49 |    0.005000 |  2.0000000000e+00   0.0000000000e+00   1.0000000000e+00 | ORI
        302 |    0.022054 |  2.0000000000e+00   1.0791023229e+00   8.8259511764e-01 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 2D

  Global number of intersections detected:         6504
    Vertex-Vertex intersections:            3594
    Other intersections:                    2910

  Joining operation is non-conforming.

  Global number of new vertices to create:       1634

  Equivalences broken for 0 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 3357 global element couples.

  Max size of a merge set of vertices: 9

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 18 faces (global).
  Join mesh cleaning done.

  Edge removed for 9 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:        701

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

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0

  After joining
     Number of cells:          22319
     Number of interior faces: 44529
     Number of boundary faces: 3850
     Number of vertices:       6063


  Joining  1 completed (0.016 s).

 -------------------------------------------------------
  Joining number 2:

  Selection criteria: "Interface_2"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.10000
    Maximum angle between joined face planes: 25.00000

  Advanced joining parameters:
    Verbosity level:                                 1
    Visualization level:                             1
    Deepest level reachable in tree building:       30
    Max boxes by leaf:                              25
    Max ratio of linked boxes / init. boxes:   5.00000
    Max ratio of boxes for distribution:       2.00000
    Merge step tolerance multiplier:           1.00000
    Pre-merge factor:                          0.05000
    Tolerance computation mode:                      1
    Intersection computation mode:                   1
    Max. number of equiv. breaks:                  500
    Max. number of subfaces by face:               200

  Before joining
     Number of cells:          22319
     Number of interior faces: 44529
     Number of boundary faces: 3850
     Number of vertices:       6063

  Global number of boundary faces selected for joining:        540

  Global number of single vertices found:      1

  Element selection successfully done.
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

       1950 |    0.005000 |  4.0000000000e+00   0.0000000000e+00   1.0000000000e+00 | ORI
       2126 |    0.022600 |  4.0000000000e+00   8.2743030619e-01   1.4186930622e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 2D

  Global number of intersections detected:         6576
    Vertex-Vertex intersections:            3662
    Other intersections:                    2914

  Joining operation is non-conforming.

  Global number of new vertices to create:       1622

  Equivalences broken for 0 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 3668 global element couples.

  Max size of a merge set of vertices: 8

  Excessive transitivity for 0 set(s) of vertices.

  Synchronization of the "single" elements after the merge step.

  Edge removed for 19 faces (global).
  Join mesh cleaning done.

  Edge removed for 9 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:        701

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

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0

  After joining
     Number of cells:          22319
     Number of interior faces: 45230
     Number of boundary faces: 3310
     Number of vertices:       6193


  Joining  2 completed (0.0161 s).

  All joining operations successfully finished:

    Wall clock time:                0.0322


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

 Halo construction with extended neighborhood
 ============================================

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

 Histogram of the number of cells per rank:

    minimum value =               5579
    maximum value =               5580

      1 : [       5579 ;       5580 ] =          4

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

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

    minimum value =               7419
    maximum value =               7779

      1 : [       7419 ;       7491 [ =          2
      2 : [       7491 ;       7563 [ =          0
      3 : [       7563 ;       7635 [ =          0
      4 : [       7635 ;       7707 [ =          1
      5 : [       7707 ;       7779 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =               1839
    maximum value =               2199

      1 : [       1839 ;       1911 [ =          2
      2 : [       1911 ;       1983 [ =          0
      3 : [       1983 ;       2055 [ =          0
      4 : [       2055 ;       2127 [ =          1
      5 : [       2127 ;       2199 ] =          1

 Histogram of the number of ghost cells
 in the standard neighborhood per rank:

    minimum value =                763
    maximum value =                911

      1 : [        763 ;        792 [ =          2
      2 : [        792 ;        822 [ =          0
      3 : [        822 ;        851 [ =          0
      4 : [        851 ;        881 [ =          0
      5 : [        881 ;        911 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =              11605
    maximum value =              11756

      1 : [      11605 ;      11635 [ =          1
      2 : [      11635 ;      11665 [ =          0
      3 : [      11665 ;      11695 [ =          1
      4 : [      11695 ;      11725 [ =          1
      5 : [      11725 ;      11756 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =                790
    maximum value =                851

      1 : [        790 ;        802 [ =          1
      2 : [        802 ;        814 [ =          0
      3 : [        814 ;        826 [ =          1
      4 : [        826 ;        838 [ =          0
      5 : [        838 ;        851 ] =          2

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                 13

      1 : [          3 ;          5 [ =      21657
      2 : [          5 ;          7 [ =        380
      3 : [          7 ;          9 [ =        170
      4 : [          9 ;         11 [ =        104
      5 : [         11 ;         13 ] =          8

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  3
    maximum value =                  3

      1 : [          3 ;          3 ] =          4

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

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

 Writing file:        mesh_output
 Finished writing:    mesh_output

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

 Partitioning 22319 cells to 4 domains on 4 ranks
   (SCOTCH_dgraphPart).

  wall-clock time: 0.136488 s

  Number of cells per domain (histogramm):
    [       5571 ;       5572 [ =          2
    [       5572 ;       5574 [ =          0
    [       5574 ;       5576 [ =          0
    [       5576 ;       5578 [ =          0
    [       5578 ;       5580 [ =          0
    [       5580 ;       5582 [ =          0
    [       5582 ;       5584 [ =          0
    [       5584 ;       5586 [ =          0
    [       5586 ;       5588 [ =          1
    [       5588 ;       5590 ] =          1

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

 Partitioning finished (0.14 s)

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

 Halo construction with extended neighborhood
 ============================================

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

 Histogram of the number of cells per rank:

    minimum value =               5571
    maximum value =               5590

      1 : [       5571 ;       5574 [ =          2
      2 : [       5574 ;       5578 [ =          0
      3 : [       5578 ;       5582 [ =          0
      4 : [       5582 ;       5586 [ =          0
      5 : [       5586 ;       5590 ] =          2

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

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

    minimum value =               6268
    maximum value =               7089

      1 : [       6268 ;       6432 [ =          2
      2 : [       6432 ;       6596 [ =          0
      3 : [       6596 ;       6760 [ =          0
      4 : [       6760 ;       6924 [ =          0
      5 : [       6924 ;       7089 ] =          2

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

 Histogram of the number of ghost cells per rank:

    minimum value =                678
    maximum value =               1518

      1 : [        678 ;        846 [ =          2
      2 : [        846 ;       1014 [ =          0
      3 : [       1014 ;       1182 [ =          0
      4 : [       1182 ;       1350 [ =          0
      5 : [       1350 ;       1518 ] =          2

 Histogram of the number of ghost cells
 in the standard neighborhood per rank:

    minimum value =                229
    maximum value =                502

      1 : [        229 ;        283 [ =          2
      2 : [        283 ;        338 [ =          0
      3 : [        338 ;        392 [ =          0
      4 : [        392 ;        447 [ =          0
      5 : [        447 ;        502 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =              11140
    maximum value =              11841

      1 : [      11140 ;      11280 [ =          2
      2 : [      11280 ;      11420 [ =          0
      3 : [      11420 ;      11560 [ =          0
      4 : [      11560 ;      11700 [ =          0
      5 : [      11700 ;      11841 ] =          2

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

 Histogram of the number of boundary faces per rank:

    minimum value =                659
    maximum value =                980

      1 : [        659 ;        723 [ =          2
      2 : [        723 ;        787 [ =          0
      3 : [        787 ;        851 [ =          0
      4 : [        851 ;        915 [ =          0
      5 : [        915 ;        980 ] =          2

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                 13

      1 : [          3 ;          5 [ =      21657
      2 : [          5 ;          7 [ =        380
      3 : [          7 ;          9 [ =        170
      4 : [          9 ;         11 [ =        104
      5 : [         11 ;         13 ] =          8

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  1
    maximum value =                  2

      1 : [          1 ;          2 ] =          4

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

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

 Renumbering mesh:

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


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =               5612
    maximum value =               6501

      1 : [       5612 ;       5789 [ =          3
      2 : [       5789 ;       5967 [ =          0
      3 : [       5967 ;       6145 [ =          0
      4 : [       6145 ;       6323 [ =          0
      5 : [       6323 ;       6501 ] =          1

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               1901
    maximum value =               2763

      1 : [       1901 ;       2073 [ =          2
      2 : [       2073 ;       2245 [ =          0
      3 : [       2245 ;       2418 [ =          0
      4 : [       2418 ;       2590 [ =          0
      5 : [       2590 ;       2763 ] =          2

 Mesh coordinates:               minimum    and maximum
                       X :  0.0000000e+00  6.0000000e+00
                       Y :  0.0000000e+00  2.0000000e+00
                       Z :  0.0000000e+00  2.0000000e+00
 Mesh
     Number of cells:          22319
     Number of interior faces: 45230
     Number of boundary faces: 3310
     Number of vertices:       6193

 Groups:
    "Inlet"
       boundary faces:          252
    "Inlet_Zone"
       cells:                  7235
    "Interface_1"
       interior faces:          701
    "Interface_2"
       interior faces:          701
    "Oulet_Zone"
       cells:                  7485
    "Outlet"
       boundary faces:          288
    "Porous_Media"
       cells:                  7599
    "Walls_Inlet_Zone"
       boundary faces:          920
    "Walls_Outlet_Zone"
       boundary faces:          916
    "Walls_Porous_Media"
       boundary faces:          934

 --- Information on the volumes
       Minimum control volume      =  2.3068374e-04
       Maximum control volume      =  3.7842073e-03
       Total volume for the domain =  2.4000000e+01

  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: 632 -->   3 %

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

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

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

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

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

 Computing geometric quantities (0.0256 s)

 Extended neighborhood reduced by non-orthogonality
 --------------------------------------------------

 Size of complete cell-cell connectivity:      1316642
 Size of filtered cell-cell conectivity:         18442
 1298200 connections removed, for a ratio of  1.4 % used
                                                             
       ALMAX  =    0.28814E+01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.


HEAD LOSS TERMS TREATMENT ACTIVATED 
                 ON   A TOTAL OF NCEPDC =       7599 CELLS


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


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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Pressure          0.0000E+00  0.0000E+00
  VelocityX         0.0000E+00  0.1000E+01
  VelocityY         0.0000E+00  0.0000E+00
  VelocityZ         0.0000E+00  0.0000E+00
  TurbEner          0.6000E-03  0.6000E-03
  Dissip            0.4590E-06  0.4590E-06
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E+01   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1000E+04  0.1000E+04
  LamVisc           0.1000E-02  0.1000E-02
  TurbVisc          0.7058E+02  0.7058E+02
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         252
Smooth wall               5        2770
Rough wall                6           0
Symmetry                  4           0
Free outlet               3         288
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.60000E+01   0.24786E-01   0.12231E+00



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252         0.000000000E+00
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         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 0.81320E+00
   Friction velocity        uet   :  0.00000E+00 0.53140E-01
   Friction velocity        uk    :  0.13416E-01 0.13416E-01
   Dimensionless distance   yplus :  0.30482E+03 0.34772E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.18531E+03     282   0.38543E+00   0.96248E+00 
c  VelocityX    0.37572E+04      20   0.26029E-01   0.26694E+02 
c  VelocityY    0.37572E+04      20   0.26029E-01   0.77362E-01 
c  VelocityZ    0.37572E+04      20   0.26029E-01   0.68535E-01 
c  TurbEner     0.54502E+01      25   0.45636E-01   0.15392E-05 
c  Dissip       0.19068E+01      31   0.16274E+00   0.11714E-04 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1098.7           52343           25177           25637
v  Velocity[x]            0.36553          1.8231         0.97434          0.9901
v  Velocity[y]           -0.23673         0.29629      0.00012887     -4.4473e-05
v  Velocity[z]           -0.23461         0.21508     -0.00021096      0.00021486
v  TurbEner            0.00058286       0.0023688      0.00062425       0.0006218
v  Dissip              4.5907e-07       0.0016088      0.00021425      0.00017065
v  TurbVisc                70.581          70.581          70.581          70.581
v  total_pressure           82578      1.5346e+05      1.1762e+05      1.1835e+05


 TIME FOR THE TIME STEP                1:        0.18949E+00

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


 INSTANT    0.200000000E+01   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399993542E+04
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 :  0.35187E+00 0.87733E+00
   Friction velocity        uet   :  0.35829E-01 0.94929E-01
   Friction velocity        uk    :  0.13415E-01 0.19089E-01
   Dimensionless distance   yplus :  0.30482E+03 0.46114E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12283E+03     430   0.33733E+00   0.96708E+00 
c  VelocityX    0.50106E+04      23   0.35890E+00   0.86231E+00 
c  VelocityY    0.50106E+04      23   0.35890E+00   0.37751E-01 
c  VelocityZ    0.50106E+04      23   0.35890E+00   0.35743E-01 
c  TurbEner     0.23440E+01      27   0.65394E-02   0.19645E-05 
c  Dissip       0.50391E+00      23   0.72224E-01   0.83621E-06 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -900.52           32800           15612           15894
v  Velocity[x]            0.53363          1.8384          1.0005         0.99634
v  Velocity[y]           -0.30551         0.25461      6.1193e-05     -5.0562e-06
v  Velocity[z]           -0.27265          0.3084      0.00026128      0.00023626
v  TurbEner            0.00040079       0.0031037      0.00067685      0.00067453
v  Dissip              4.5767e-07       0.0020139      0.00017336      0.00013912
v  TurbVisc              0.020139          70.575           18.11          21.205
v  total_pressure           83126      1.3366e+05      1.0805e+05      1.0861e+05


 TIME FOR THE TIME STEP                2:        0.17878E+00

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


 INSTANT    0.300000000E+01   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001714E+04
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 :  0.23407E+00 0.82752E+00
   Friction velocity        uet   :  0.24279E-01 0.75102E-01
   Friction velocity        uk    :  0.10965E-01 0.28711E-01
   Dimensionless distance   yplus :  0.26522E+03 0.70544E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.91611E+02     366   0.96254E-01   0.41219E+00 
c  VelocityX    0.54417E+04      22   0.18246E+00   0.25087E+00 
c  VelocityY    0.54417E+04      22   0.18246E+00   0.64723E-02 
c  VelocityZ    0.54417E+04      22   0.18246E+00   0.62158E-02 
c  TurbEner     0.24707E+01      27   0.37999E-02   0.84506E-06 
c  Dissip       0.44274E+00      23   0.34223E-01   0.84595E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -466.59           47216           22961           23383
v  Velocity[x]             0.4086           1.835         0.96269          0.9609
v  Velocity[y]           -0.37375         0.61281      0.00021138      0.00011526
v  Velocity[z]           -0.37445          0.4236      0.00021929      0.00019301
v  TurbEner            0.00029235       0.0033886      0.00073163      0.00073226
v  Dissip              4.6031e-07       0.0019059      0.00015818      0.00012745
v  TurbVisc              0.017096          71.383          15.001          17.465
v  total_pressure           82926      1.4881e+05       1.154e+05       1.161e+05


 TIME FOR THE TIME STEP                3:        0.16678E+00

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


 INSTANT    0.400000000E+01   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004180E+04
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 :  0.15431E+00 0.95150E+00
   Friction velocity        uet   :  0.14617E-01 0.93856E-01
   Friction velocity        uk    :  0.93651E-02 0.31110E-01
   Dimensionless distance   yplus :  0.22990E+03 0.77319E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55629E+02     331   0.42965E-01   0.20607E+00 
c  VelocityX    0.54337E+04      20   0.82338E-01   0.67197E-01 
c  VelocityY    0.54337E+04      20   0.82338E-01   0.17741E-02 
c  VelocityZ    0.54337E+04      20   0.82338E-01   0.18275E-02 
c  TurbEner     0.25556E+01      27   0.27607E-02   0.64578E-06 
c  Dissip       0.35406E+00      23   0.38496E-01   0.75340E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -131.17           54030           26468           26954
v  Velocity[x]            0.32039          2.0215          0.9372          0.9377
v  Velocity[y]           -0.37125         0.62241      0.00011447      1.3231e-05
v  Velocity[z]           -0.43831          0.4281      9.9903e-05      0.00010306
v  TurbEner             0.0002258       0.0035003      0.00077708      0.00078464
v  Dissip              4.6243e-07       0.0020097      0.00014049       0.0001144
v  TurbVisc              0.015212          71.422          12.664          14.702
v  total_pressure           83042      1.5588e+05      1.1891e+05      1.1967e+05


 TIME FOR THE TIME STEP                4:        0.15533E+00

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


 INSTANT    0.500000000E+01   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400005074E+04
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 :  0.12338E+00 0.84079E+00
   Friction velocity        uet   :  0.11345E-01 0.80654E-01
   Friction velocity        uk    :  0.82304E-02 0.31991E-01
   Dimensionless distance   yplus :  0.20193E+03 0.79768E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37251E+02     295   0.19280E-01   0.12447E+00 
c  VelocityX    0.53679E+04      19   0.35290E-01   0.23030E-01 
c  VelocityY    0.53679E+04      19   0.35290E-01   0.60401E-03 
c  VelocityZ    0.53679E+04      19   0.35290E-01   0.68899E-03 
c  TurbEner     0.26303E+01      26   0.21009E-02   0.53626E-06 
c  Dissip       0.29422E+00      23   0.38718E-01   0.70554E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -162.88           56304           27599           28107
v  Velocity[x]            0.29131          2.0743         0.92193         0.92284
v  Velocity[y]           -0.37784         0.59832      9.7976e-05      1.4404e-05
v  Velocity[z]           -0.42827         0.39019      2.2404e-05      2.2452e-05
v  TurbEner            0.00018447       0.0035448      0.00082044      0.00083587
v  Dissip               4.665e-07       0.0019886      0.00012793      0.00010558
v  TurbVisc              0.014178          70.924          10.815          12.546
v  total_pressure           83046      1.5822e+05      1.2004e+05      1.2082e+05


 TIME FOR THE TIME STEP                5:        0.14702E+00

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


 INSTANT    0.600000000E+01   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400005410E+04
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 :  0.13769E+00 0.90144E+00
   Friction velocity        uet   :  0.12645E-01 0.79698E-01
   Friction velocity        uk    :  0.74391E-02 0.32335E-01
   Dimensionless distance   yplus :  0.18100E+03 0.80680E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26278E+02     227   0.99120E-02   0.84180E-01 
c  VelocityX    0.52189E+04      17   0.13530E-01   0.66051E-02 
c  VelocityY    0.52189E+04      17   0.13530E-01   0.29896E-03 
c  VelocityZ    0.52189E+04      17   0.13530E-01   0.37258E-03 
c  TurbEner     0.27037E+01      26   0.15575E-02   0.45733E-06 
c  Dissip       0.26742E+00      24   0.26616E-01   0.38045E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.28           56720           27821           28333
v  Velocity[x]            0.25604          1.7221         0.91512           0.916
v  Velocity[y]           -0.37253         0.66702      5.5082e-05      2.0407e-06
v  Velocity[z]           -0.40226          0.4326     -2.7559e-05     -3.0207e-05
v  TurbEner            0.00015642       0.0035634      0.00086582      0.00088837
v  Dissip               4.733e-07         0.00177      0.00012232      0.00010209
v  TurbVisc              0.013622          70.255          9.3151          10.818
v  total_pressure           83056      1.5866e+05      1.2026e+05      1.2105e+05


 TIME FOR THE TIME STEP                6:        0.13363E+00

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


 INSTANT    0.700000000E+01   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400005810E+04
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 :  0.20268E+00 0.92491E+00
   Friction velocity        uet   :  0.19261E-01 0.76551E-01
   Friction velocity        uk    :  0.68502E-02 0.32454E-01
   Dimensionless distance   yplus :  0.16747E+03 0.80974E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.18957E+02     216   0.65131E-02   0.59460E-01 
c  VelocityX    0.50772E+04      16   0.76492E-02   0.22957E-02 
c  VelocityY    0.50772E+04      16   0.76492E-02   0.20686E-03 
c  VelocityZ    0.50772E+04      16   0.76492E-02   0.23757E-03 
c  TurbEner     0.27800E+01      26   0.11977E-02   0.40056E-06 
c  Dissip       0.26134E+00      24   0.17993E-01   0.22868E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -202.88           56402           27674           28183
v  Velocity[x]            0.31027          1.8655         0.91187         0.91274
v  Velocity[y]           -0.38827         0.70891      4.9528e-05       1.694e-05
v  Velocity[z]           -0.41232         0.46377     -7.0745e-05     -8.1103e-05
v  TurbEner            0.00013947       0.0035713      0.00091281      0.00094159
v  Dissip               4.838e-07       0.0016515      0.00012128      0.00010212
v  TurbVisc              0.013522           69.24          8.0883          9.4105
v  total_pressure           83028      1.5838e+05      1.2011e+05       1.209e+05


 TIME FOR THE TIME STEP                7:        0.13127E+00

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


 INSTANT    0.800000000E+01   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399995480E+04
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 :  0.16693E+00 0.99024E+00
   Friction velocity        uet   :  0.15958E-01 0.80988E-01
   Friction velocity        uk    :  0.64683E-02 0.32505E-01
   Dimensionless distance   yplus :  0.15814E+03 0.81090E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15769E+02     225   0.53905E-02   0.48930E-01 
c  VelocityX    0.49593E+04      16   0.83165E-02   0.14011E-02 
c  VelocityY    0.49593E+04      16   0.83165E-02   0.15351E-03 
c  VelocityZ    0.49593E+04      16   0.83165E-02   0.18199E-03 
c  TurbEner     0.28580E+01      26   0.96353E-03   0.35832E-06 
c  Dissip       0.26459E+00      23   0.12666E-01   0.15155E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -184.33           55950           27474           27980
v  Velocity[x]            0.26922          1.9878         0.91038         0.91129
v  Velocity[y]           -0.40034         0.70027      1.9846e-05      1.1611e-05
v  Velocity[z]            -0.4152         0.46911     -0.00010884     -0.00012455
v  TurbEner             0.0001335       0.0035748      0.00096116      0.00099523
v  Dissip              4.9914e-07       0.0016713      0.00012295      0.00010424
v  TurbVisc              0.014367          67.641          7.0816          8.2512
v  total_pressure           83030      1.5797e+05      1.1991e+05       1.207e+05


 TIME FOR THE TIME STEP                8:        0.13248E+00

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


 INSTANT    0.900000000E+01   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994331E+04
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 :  0.14474E+00 0.10902E+01
   Friction velocity        uet   :  0.13797E-01 0.77604E-01
   Friction velocity        uk    :  0.63285E-02 0.32525E-01
   Dimensionless distance   yplus :  0.15472E+03 0.81128E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13792E+02     225   0.41471E-02   0.42432E-01 
c  VelocityX    0.48657E+04      15   0.74740E-02   0.13365E-02 
c  VelocityY    0.48657E+04      15   0.74740E-02   0.12026E-03 
c  VelocityZ    0.48657E+04      15   0.74740E-02   0.14961E-03 
c  TurbEner     0.29370E+01      25   0.80879E-03   0.32563E-06 
c  Dissip       0.27175E+00      23   0.97407E-02   0.11041E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -204.24           55521           27280           27783
v  Velocity[x]            0.30647          2.0874         0.90946          0.9104
v  Velocity[y]           -0.38626         0.70935      1.3152e-05       1.462e-05
v  Velocity[z]            -0.4097         0.47101     -0.00014732      -0.0001648
v  TurbEner            0.00013653       0.0035764       0.0010105        0.001049
v  Dissip              5.2073e-07       0.0017609      0.00012623      0.00010758
v  TurbVisc              0.016343          65.564          6.2528          7.2959
v  total_pressure           83040      1.5758e+05      1.1972e+05       1.205e+05


 TIME FOR THE TIME STEP                9:        0.13156E+00

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994132E+04
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 :  0.13655E+00 0.11631E+01
   Friction velocity        uet   :  0.12880E-01 0.79514E-01
   Friction velocity        uk    :  0.63999E-02 0.32534E-01
   Dimensionless distance   yplus :  0.15646E+03 0.81142E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13235E+02     222   0.34388E-02   0.40438E-01 
c  VelocityX    0.47898E+04      15   0.71592E-02   0.98313E-03 
c  VelocityY    0.47898E+04      15   0.71592E-02   0.11880E-03 
c  VelocityZ    0.47898E+04      15   0.71592E-02   0.12860E-03 
c  TurbEner     0.30162E+01      25   0.69427E-03   0.29961E-06 
c  Dissip       0.28036E+00      23   0.76947E-02   0.85562E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -193.38           55191           27115           27615
v  Velocity[x]            0.26279          2.1319         0.90871         0.90974
v  Velocity[y]           -0.39167         0.70308      6.1934e-06      1.9258e-05
v  Velocity[z]           -0.39801          0.4886     -0.00017468     -0.00020078
v  TurbEner            0.00014724       0.0035776       0.0010608       0.0011027
v  Dissip              5.5038e-07       0.0018065      0.00013051      0.00011167
v  TurbVisc              0.019475          62.914          5.5671          6.5109
v  total_pressure           83041      1.5723e+05      1.1956e+05      1.2033e+05


 TIME FOR THE TIME STEP               10:        0.13146E+00

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


 INSTANT    0.110000000E+02   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994587E+04
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 :  0.13478E+00 0.12350E+01
   Friction velocity        uet   :  0.12571E-01 0.79024E-01
   Friction velocity        uk    :  0.66462E-02 0.32538E-01
   Dimensionless distance   yplus :  0.16249E+03 0.81147E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12970E+02     219   0.37166E-02   0.39273E-01 
c  VelocityX    0.47264E+04      15   0.76780E-02   0.12028E-02 
c  VelocityY    0.47264E+04      15   0.76780E-02   0.12439E-03 
c  VelocityZ    0.47264E+04      15   0.76780E-02   0.11838E-03 
c  TurbEner     0.30953E+01      25   0.62578E-03   0.27876E-06 
c  Dissip       0.29022E+00      23   0.65561E-02   0.72566E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -208.49           54873           26967           27465
v  Velocity[x]            0.30299          2.1886         0.90787         0.90899
v  Velocity[y]           -0.39828         0.71006      2.0213e-05      4.0502e-05
v  Velocity[z]           -0.38841         0.48925     -0.00020758     -0.00022872
v  TurbEner            0.00016461       0.0035784       0.0011119       0.0011565
v  Dissip              5.9056e-07       0.0017763      0.00013546      0.00011626
v  TurbVisc              0.021734          59.742          5.0045          5.8671
v  total_pressure           83045      1.5692e+05      1.1941e+05      1.2018e+05


 TIME FOR THE TIME STEP               11:        0.13072E+00

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


 INSTANT    0.120000000E+02   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994596E+04
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 :  0.13858E+00 0.11594E+01
   Friction velocity        uet   :  0.12657E-01 0.80406E-01
   Friction velocity        uk    :  0.70273E-02 0.32539E-01
   Dimensionless distance   yplus :  0.17180E+03 0.81148E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13480E+02     216   0.41882E-02   0.40499E-01 
c  VelocityX    0.46715E+04      15   0.79673E-02   0.10032E-02 
c  VelocityY    0.46715E+04      15   0.79673E-02   0.99215E-04 
c  VelocityZ    0.46715E+04      15   0.79673E-02   0.13266E-03 
c  TurbEner     0.31741E+01      25   0.59262E-03   0.26245E-06 
c  Dissip       0.30055E+00      23   0.56231E-02   0.66103E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -195.63           54570           26832           27328
v  Velocity[x]            0.26297          2.2143         0.90714         0.90832
v  Velocity[y]            -0.3746         0.69839      1.3024e-05      3.6762e-05
v  Velocity[z]           -0.37978         0.48354     -0.00025141     -0.00027678
v  TurbEner            0.00016431       0.0035788        0.001164       0.0012102
v  Dissip              6.4459e-07       0.0018226      0.00014093      0.00012121
v  TurbVisc              0.023348          56.143          4.5519           5.341
v  total_pressure           83060      1.5663e+05      1.1927e+05      1.2004e+05


 TIME FOR THE TIME STEP               12:        0.13161E+00

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


 INSTANT    0.130000000E+02   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994843E+04
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 :  0.14571E+00 0.12735E+01
   Friction velocity        uet   :  0.12860E-01 0.78565E-01
   Friction velocity        uk    :  0.70210E-02 0.32540E-01
   Dimensionless distance   yplus :  0.17497E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12614E+02     216   0.45259E-02   0.37537E-01 
c  VelocityX    0.46236E+04      15   0.76709E-02   0.87500E-03 
c  VelocityY    0.46236E+04      15   0.76709E-02   0.99238E-04 
c  VelocityZ    0.46236E+04      15   0.76709E-02   0.19531E-03 
c  TurbEner     0.32524E+01      24   0.59671E-03   0.24829E-06 
c  Dissip       0.31186E+00      23   0.50742E-02   0.63727E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -207.69           54324           26703           27198
v  Velocity[x]            0.30396          2.2349         0.90651         0.90778
v  Velocity[y]           -0.38888         0.70354      3.1791e-05      5.4217e-05
v  Velocity[z]           -0.37339         0.49785     -0.00029556     -0.00032011
v  TurbEner            0.00016847       0.0036661       0.0012166       0.0012638
v  Dissip              7.1679e-07       0.0022078      0.00014674      0.00012637
v  TurbVisc              0.026711          52.232          4.1948          4.9156
v  total_pressure           83056      1.5635e+05      1.1914e+05      1.1991e+05


 TIME FOR THE TIME STEP               13:        0.13229E+00

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


 INSTANT    0.140000000E+02   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994801E+04
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 :  0.15603E+00 0.12545E+01
   Friction velocity        uet   :  0.13148E-01 0.80941E-01
   Friction velocity        uk    :  0.71092E-02 0.32541E-01
   Dimensionless distance   yplus :  0.17716E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10919E+02     216   0.41671E-02   0.32341E-01 
c  VelocityX    0.45821E+04      14   0.89830E-02   0.74929E-03 
c  VelocityY    0.45821E+04      14   0.89830E-02   0.90806E-04 
c  VelocityZ    0.45821E+04      14   0.89830E-02   0.11513E-03 
c  TurbEner     0.33303E+01      24   0.64224E-03   0.23870E-06 
c  Dissip       0.32433E+00      23   0.45530E-02   0.63800E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -199.56           54064           26587           27081
v  Velocity[x]            0.26352          2.2431         0.90612         0.90746
v  Velocity[y]            -0.3978         0.69361      3.3872e-05      5.3867e-05
v  Velocity[z]           -0.36824          0.4929     -0.00036611     -0.00040372
v  TurbEner            0.00018339       0.0042994       0.0012699       0.0013175
v  Dissip              8.1247e-07       0.0026527      0.00015284      0.00013171
v  TurbVisc              0.029257          48.132          3.9172          4.5777
v  total_pressure           83059      1.5611e+05      1.1903e+05       1.198e+05


 TIME FOR THE TIME STEP               14:        0.13156E+00

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


 INSTANT    0.150000000E+02   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994973E+04
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 :  0.16735E+00 0.13089E+01
   Friction velocity        uet   :  0.13396E-01 0.79275E-01
   Friction velocity        uk    :  0.74174E-02 0.32541E-01
   Dimensionless distance   yplus :  0.18421E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.99694E+01     206   0.37410E-02   0.29499E-01 
c  VelocityX    0.45474E+04      15   0.89016E-02   0.92179E-03 
c  VelocityY    0.45474E+04      15   0.89016E-02   0.75071E-04 
c  VelocityZ    0.45474E+04      15   0.89016E-02   0.82979E-04 
c  TurbEner     0.34077E+01      24   0.66802E-03   0.23121E-06 
c  Dissip       0.33883E+00      23   0.41968E-02   0.65358E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -210.65           53866           26486           26979
v  Velocity[x]            0.30301          2.2575         0.90578         0.90718
v  Velocity[y]           -0.37495         0.69528      5.5767e-05      6.8403e-05
v  Velocity[z]           -0.36575          0.4845     -0.00045246     -0.00049316
v  TurbEner            0.00019232       0.0050211       0.0013237       0.0013712
v  Dissip              9.1996e-07       0.0031867      0.00015917      0.00013717
v  TurbVisc              0.031625          43.955          3.7044          4.3149
v  total_pressure           83071       1.559e+05      1.1893e+05      1.1969e+05


 TIME FOR THE TIME STEP               15:        0.12971E+00

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


 INSTANT    0.160000000E+02   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399993269E+04
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 :  0.17897E+00 0.11621E+01
   Friction velocity        uet   :  0.13652E-01 0.81861E-01
   Friction velocity        uk    :  0.75959E-02 0.32541E-01
   Dimensionless distance   yplus :  0.18638E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.93569E+01     190   0.27358E-02   0.27710E-01 
c  VelocityX    0.45194E+04      14   0.80628E-02   0.70171E-03 
c  VelocityY    0.45194E+04      14   0.80628E-02   0.60018E-04 
c  VelocityZ    0.45194E+04      14   0.80628E-02   0.98967E-04 
c  TurbEner     0.34842E+01      24   0.65145E-03   0.22261E-06 
c  Dissip       0.35495E+00      23   0.38380E-02   0.67339E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -196.51           53686           26401           26893
v  Velocity[x]            0.26731          2.2485         0.90557         0.90703
v  Velocity[y]           -0.38876         0.68306      6.1658e-05      6.7332e-05
v  Velocity[z]           -0.36254         0.49814     -0.00053798     -0.00059517
v  TurbEner             0.0002048       0.0058451       0.0013776       0.0014248
v  Dissip              1.0235e-06       0.0038132      0.00016562       0.0001427
v  TurbVisc              0.034615          39.813          3.5446          4.1154
v  total_pressure           83066      1.5572e+05      1.1884e+05      1.1961e+05


 TIME FOR THE TIME STEP               16:        0.13787E+00

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


 INSTANT    0.170000000E+02   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399993823E+04
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 :  0.19104E+00 0.12239E+01
   Friction velocity        uet   :  0.13996E-01 0.75927E-01
   Friction velocity        uk    :  0.78384E-02 0.32541E-01
   Dimensionless distance   yplus :  0.19233E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.96762E+01     183   0.24038E-02   0.28705E-01 
c  VelocityX    0.44979E+04      14   0.73110E-02   0.65371E-03 
c  VelocityY    0.44979E+04      14   0.73110E-02   0.68679E-04 
c  VelocityZ    0.44979E+04      14   0.73110E-02   0.17200E-03 
c  TurbEner     0.35602E+01      24   0.65081E-03   0.21776E-06 
c  Dissip       0.37343E+00      23   0.36775E-02   0.73318E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -204.17           53559           26330           26820
v  Velocity[x]            0.25185          2.0578         0.90539         0.90691
v  Velocity[y]           -0.39724         0.68482        9.34e-05      8.0672e-05
v  Velocity[z]           -0.36187         0.49155     -0.00061492     -0.00068648
v  TurbEner            0.00022621       0.0069521       0.0014317       0.0014784
v  Dissip              1.1475e-06       0.0047121      0.00017216      0.00014827
v  TurbVisc              0.039635          35.785          3.4278          3.9678
v  total_pressure           83067      1.5558e+05      1.1877e+05      1.1954e+05


 TIME FOR THE TIME STEP               17:        0.12436E+00

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


 INSTANT    0.180000000E+02   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399994564E+04
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 :  0.19833E+00 0.12084E+01
   Friction velocity        uet   :  0.14077E-01 0.82989E-01
   Friction velocity        uk    :  0.82379E-02 0.32541E-01
   Dimensionless distance   yplus :  0.20138E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.85282E+01     180   0.24196E-02   0.25386E-01 
c  VelocityX    0.44823E+04      14   0.73045E-02   0.56608E-03 
c  VelocityY    0.44823E+04      14   0.73045E-02   0.57856E-04 
c  VelocityZ    0.44823E+04      14   0.73045E-02   0.83864E-04 
c  TurbEner     0.36352E+01      24   0.63262E-03   0.21228E-06 
c  Dissip       0.39017E+00      23   0.30712E-02   0.58026E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -192.63           53448           26277           26766
v  Velocity[x]            0.24825          2.1102         0.90529         0.90687
v  Velocity[y]           -0.37426         0.67398       0.0001127      8.5913e-05
v  Velocity[z]           -0.36031         0.48146     -0.00070561     -0.00078927
v  TurbEner            0.00022892       0.0074834       0.0014861       0.0015321
v  Dissip              1.2943e-06       0.0051669      0.00017874      0.00015386
v  TurbVisc              0.045804          31.981          3.3464          3.8621
v  total_pressure           83079      1.5549e+05      1.1872e+05      1.1948e+05


 TIME FOR THE TIME STEP               18:        0.12311E+00

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


 INSTANT    0.190000000E+02   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399995375E+04
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 :  0.20483E+00 0.12531E+01
   Friction velocity        uet   :  0.14193E-01 0.76476E-01
   Friction velocity        uk    :  0.82872E-02 0.32541E-01
   Dimensionless distance   yplus :  0.20227E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.74542E+01     153   0.22792E-02   0.22265E-01 
c  VelocityX    0.44718E+04      14   0.75146E-02   0.48875E-03 
c  VelocityY    0.44718E+04      14   0.75146E-02   0.43893E-04 
c  VelocityZ    0.44718E+04      14   0.75146E-02   0.55115E-04 
c  TurbEner     0.37100E+01      24   0.62847E-03   0.20928E-06 
c  Dissip       0.41099E+00      23   0.29436E-02   0.64690E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -204.95           53368           26235           26723
v  Velocity[x]            0.24925          2.1541         0.90521         0.90685
v  Velocity[y]           -0.39285         0.68314       0.0001406      9.5697e-05
v  Velocity[z]           -0.35883         0.49596     -0.00081946     -0.00091248
v  TurbEner            0.00023115       0.0082376       0.0015407       0.0015861
v  Dissip               1.463e-06       0.0058421      0.00018544      0.00015952
v  TurbVisc              0.051423          28.466          3.2934          3.7901
v  total_pressure           83072      1.5541e+05      1.1868e+05      1.1944e+05


 TIME FOR THE TIME STEP               19:        0.11720E+00

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


 INSTANT    0.200000000E+02   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399995382E+04
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 :  0.20897E+00 0.12170E+01
   Friction velocity        uet   :  0.14216E-01 0.83505E-01
   Friction velocity        uk    :  0.83274E-02 0.32541E-01
   Dimensionless distance   yplus :  0.20325E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.81116E+01     145   0.26351E-02   0.24286E-01 
c  VelocityX    0.44652E+04      14   0.84195E-02   0.53079E-03 
c  VelocityY    0.44652E+04      14   0.84195E-02   0.43868E-04 
c  VelocityZ    0.44652E+04      14   0.84195E-02   0.63950E-04 
c  TurbEner     0.37850E+01      24   0.61659E-03   0.20767E-06 
c  Dissip       0.43563E+00      23   0.28319E-02   0.73408E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -192.02           53323           26207           26693
v  Velocity[x]            0.25323          2.1638          0.9052         0.90691
v  Velocity[y]           -0.39441         0.67869      0.00015915      9.7786e-05
v  Velocity[z]            -0.3431         0.49233      -0.0009113      -0.0010215
v  TurbEner             0.0002342       0.0091026       0.0015956       0.0016403
v  Dissip              1.6713e-06       0.0066512      0.00019231      0.00016533
v  TurbVisc              0.054038          25.417          3.2629          3.7453
v  total_pressure           83073      1.5537e+05      1.1865e+05      1.1941e+05


 TIME FOR THE TIME STEP               20:        0.11591E+00

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


 INSTANT    0.210000000E+02   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399995874E+04
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 :  0.22512E+00 0.12001E+01
   Friction velocity        uet   :  0.15101E-01 0.76289E-01
   Friction velocity        uk    :  0.83821E-02 0.32541E-01
   Dimensionless distance   yplus :  0.20459E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.81386E+01     127   0.28216E-02   0.24494E-01 
c  VelocityX    0.44624E+04      14   0.78230E-02   0.56175E-03 
c  VelocityY    0.44624E+04      14   0.78230E-02   0.54100E-04 
c  VelocityZ    0.44624E+04      14   0.78230E-02   0.14248E-03 
c  TurbEner     0.38603E+01      24   0.61270E-03   0.20752E-06 
c  Dissip       0.46453E+00      23   0.27570E-02   0.81006E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -196.52           53316           26190           26675
v  Velocity[x]            0.25673          2.1739         0.90523           0.907
v  Velocity[y]           -0.37508         0.69985      0.00020044      0.00011541
v  Velocity[z]           -0.36686         0.48303     -0.00098798      -0.0011019
v  TurbEner            0.00023903        0.010065       0.0016509       0.0016951
v  Dissip              1.9415e-06        0.007617       0.0001994      0.00017132
v  TurbVisc               0.05698          22.464          3.2498           3.722
v  total_pressure           83083      1.5535e+05      1.1863e+05      1.1939e+05


 TIME FOR THE TIME STEP               21:        0.11178E+00

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


 INSTANT    0.220000000E+02   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997289E+04
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 :  0.22289E+00 0.12583E+01
   Friction velocity        uet   :  0.14772E-01 0.83422E-01
   Friction velocity        uk    :  0.84682E-02 0.32541E-01
   Dimensionless distance   yplus :  0.20669E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75104E+01     121   0.30021E-02   0.22689E-01 
c  VelocityX    0.44626E+04      15   0.66045E-02   0.49543E-03 
c  VelocityY    0.44626E+04      15   0.66045E-02   0.45290E-04 
c  VelocityZ    0.44626E+04      15   0.66045E-02   0.73804E-04 
c  TurbEner     0.39352E+01      24   0.58236E-03   0.20322E-06 
c  Dissip       0.49772E+00      22   0.27113E-02   0.90629E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -186.14           53319           26184           26669
v  Velocity[x]            0.25954          2.1863         0.90527          0.9071
v  Velocity[y]           -0.39111         0.69741      0.00022366      0.00012379
v  Velocity[z]           -0.36772         0.47057      -0.0010823      -0.0012074
v  TurbEner            0.00024644        0.010984       0.0017064         0.00175
v  Dissip              2.2881e-06       0.0086614      0.00020671      0.00017749
v  TurbVisc              0.060536          19.546          3.2507          3.7159
v  total_pressure           83087      1.5535e+05      1.1862e+05      1.1938e+05


 TIME FOR THE TIME STEP               22:        0.11054E+00

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


 INSTANT    0.230000000E+02   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998020E+04
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 :  0.22931E+00 0.12238E+01
   Friction velocity        uet   :  0.15052E-01 0.76315E-01
   Friction velocity        uk    :  0.85983E-02 0.32541E-01
   Dimensionless distance   yplus :  0.20986E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67029E+01     122   0.28686E-02   0.20340E-01 
c  VelocityX    0.44654E+04      14   0.72109E-02   0.42606E-03 
c  VelocityY    0.44654E+04      14   0.72109E-02   0.35053E-04 
c  VelocityZ    0.44654E+04      14   0.72109E-02   0.47623E-04 
c  TurbEner     0.40102E+01      23   0.54859E-03   0.20029E-06 
c  Dissip       0.53554E+00      22   0.26800E-02   0.10048E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -194.83           53340           26186           26670
v  Velocity[x]            0.26203          2.1958         0.90533         0.90722
v  Velocity[y]           -0.39291         0.71207      0.00025404      0.00013686
v  Velocity[z]            -0.3782         0.49088      -0.0011647      -0.0012963
v  TurbEner            0.00025704        0.011882       0.0017622       0.0018052
v  Dissip              2.6838e-06       0.0098199      0.00021429      0.00018389
v  TurbVisc              0.064815          16.908          3.2627          3.7232
v  total_pressure           83085      1.5537e+05      1.1863e+05      1.1939e+05


 TIME FOR THE TIME STEP               23:        0.11087E+00

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


 INSTANT    0.240000000E+02   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000034E+04
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 :  0.22981E+00 0.12770E+01
   Friction velocity        uet   :  0.14944E-01 0.82965E-01
   Friction velocity        uk    :  0.87814E-02 0.32541E-01
   Dimensionless distance   yplus :  0.21433E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.76974E+01     141   0.27764E-02   0.23461E-01 
c  VelocityX    0.44702E+04      14   0.75043E-02   0.46826E-03 
c  VelocityY    0.44702E+04      14   0.75043E-02   0.41643E-04 
c  VelocityZ    0.44702E+04      14   0.75043E-02   0.57338E-04 
c  TurbEner     0.40845E+01      23   0.51655E-03   0.19539E-06 
c  Dissip       0.57782E+00      22   0.26954E-02   0.11341E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.55           53369           26197           26681
v  Velocity[x]            0.26424          2.1884         0.90545          0.9074
v  Velocity[y]           -0.41349         0.71061      0.00027702      0.00015201
v  Velocity[z]           -0.38788          0.5077      -0.0012017      -0.0013463
v  TurbEner            0.00027115        0.012777       0.0018178       0.0018604
v  Dissip              3.0126e-06        0.011092       0.0002221      0.00019048
v  TurbVisc                0.0698           14.72          3.2836          3.7408
v  total_pressure           83075      1.5541e+05      1.1864e+05       1.194e+05


 TIME FOR THE TIME STEP               24:        0.11506E+00

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


 INSTANT    0.250000000E+02   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001570E+04
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 :  0.23057E+00 0.11967E+01
   Friction velocity        uet   :  0.14865E-01 0.75955E-01
   Friction velocity        uk    :  0.90191E-02 0.32541E-01
   Dimensionless distance   yplus :  0.22013E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.76468E+01     143   0.25192E-02   0.23403E-01 
c  VelocityX    0.44765E+04      14   0.68040E-02   0.46576E-03 
c  VelocityY    0.44765E+04      14   0.68040E-02   0.58636E-04 
c  VelocityZ    0.44765E+04      14   0.68040E-02   0.13788E-03 
c  TurbEner     0.41585E+01      23   0.49317E-03   0.18997E-06 
c  Dissip       0.62662E+00      22   0.27859E-02   0.12632E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -189           53437           26215           26698
v  Velocity[x]            0.26587          2.1989         0.90553         0.90752
v  Velocity[y]           -0.40402         0.72227      0.00031777      0.00017805
v  Velocity[z]           -0.39661         0.50237      -0.0012537      -0.0014081
v  TurbEner            0.00028856        0.013681       0.0018734       0.0019157
v  Dissip              3.3865e-06        0.012536      0.00023017      0.00019731
v  TurbVisc              0.075332           13.29          3.3114          3.7664
v  total_pressure           83082      1.5545e+05      1.1865e+05      1.1941e+05


 TIME FOR THE TIME STEP               25:        0.11607E+00

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


 INSTANT    0.260000000E+02   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002653E+04
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 :  0.23105E+00 0.12916E+01
   Friction velocity        uet   :  0.14772E-01 0.82724E-01
   Friction velocity        uk    :  0.93042E-02 0.32560E-01
   Dimensionless distance   yplus :  0.22709E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69641E+01     147   0.23508E-02   0.21419E-01 
c  VelocityX    0.44839E+04      13   0.69403E-02   0.41206E-03 
c  VelocityY    0.44839E+04      13   0.69403E-02   0.49198E-04 
c  VelocityZ    0.44839E+04      13   0.69403E-02   0.70347E-04 
c  TurbEner     0.42318E+01      23   0.47546E-03   0.18487E-06 
c  Dissip       0.67988E+00      22   0.28475E-02   0.14567E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.82           53479           26239           26723
v  Velocity[x]            0.26832          2.1951         0.90571         0.90773
v  Velocity[y]           -0.41493         0.71522      0.00033879      0.00018991
v  Velocity[z]           -0.40508         0.51461      -0.0012954      -0.0014592
v  TurbEner            0.00030894        0.014462        0.001929       0.0019709
v  Dissip              3.8377e-06        0.014013      0.00023855      0.00020438
v  TurbVisc              0.081082          12.006          3.3448          3.7982
v  total_pressure           83074      1.5551e+05      1.1868e+05      1.1944e+05


 TIME FOR THE TIME STEP               26:        0.11618E+00

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


 INSTANT    0.270000000E+02   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400003602E+04
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 :  0.23147E+00 0.12364E+01
   Friction velocity        uet   :  0.14679E-01 0.75819E-01
   Friction velocity        uk    :  0.96272E-02 0.32716E-01
   Dimensionless distance   yplus :  0.23498E+03 0.81149E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.74153E+01     149   0.21447E-02   0.22917E-01 
c  VelocityX    0.44923E+04      13   0.73858E-02   0.37377E-03 
c  VelocityY    0.44923E+04      13   0.73858E-02   0.47156E-04 
c  VelocityZ    0.44923E+04      13   0.73858E-02   0.42256E-04 
c  TurbEner     0.43043E+01      23   0.46198E-03   0.17898E-06 
c  Dissip       0.74000E+00      22   0.29075E-02   0.15906E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -186.76           53544           26267           26751
v  Velocity[x]            0.26982          2.2096         0.90585         0.90789
v  Velocity[y]           -0.39297         0.72775      0.00038193      0.00022273
v  Velocity[z]             -0.411         0.51225      -0.0013355      -0.0014991
v  TurbEner            0.00033164        0.015178       0.0019843       0.0020261
v  Dissip              4.4178e-06        0.015637      0.00024719      0.00021168
v  TurbVisc              0.086723          11.013          3.3823          3.8349
v  total_pressure           83081      1.5558e+05      1.1871e+05      1.1947e+05


 TIME FOR THE TIME STEP               27:        0.11667E+00

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


 INSTANT    0.280000000E+02   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004390E+04
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 :  0.23158E+00 0.13052E+01
   Friction velocity        uet   :  0.14597E-01 0.82490E-01
   Friction velocity        uk    :  0.99745E-02 0.32982E-01
   Dimensionless distance   yplus :  0.24267E+03 0.81281E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71933E+01     149   0.20265E-02   0.22335E-01 
c  VelocityX    0.45008E+04      13   0.74991E-02   0.52523E-03 
c  VelocityY    0.45008E+04      13   0.74991E-02   0.47295E-04 
c  VelocityZ    0.45008E+04      13   0.74991E-02   0.57626E-04 
c  TurbEner     0.43736E+01      23   0.46207E-03   0.17306E-06 
c  Dissip       0.79671E+00      22   0.34504E-02   0.19948E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.17           53590           26299           26784
v  Velocity[x]            0.27182          2.0197         0.90601         0.90805
v  Velocity[y]           -0.40494         0.72249       0.0003895      0.00022455
v  Velocity[z]           -0.41631         0.51841      -0.0013661      -0.0015371
v  TurbEner            0.00035586        0.016215       0.0020393        0.002081
v  Dissip              4.7964e-06        0.017884      0.00025606      0.00021917
v  TurbVisc              0.092023          11.013          3.4229          3.8753
v  total_pressure           83079      1.5564e+05      1.1874e+05       1.195e+05


 TIME FOR THE TIME STEP               28:        0.11663E+00

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


 INSTANT    0.290000000E+02   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004817E+04
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 :  0.23166E+00 0.12021E+01
   Friction velocity        uet   :  0.14532E-01 0.75512E-01
   Friction velocity        uk    :  0.10332E-01 0.33187E-01
   Dimensionless distance   yplus :  0.25073E+03 0.81786E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67198E+01     149   0.17901E-02   0.20964E-01 
c  VelocityX    0.45096E+04      13   0.72770E-02   0.40518E-03 
c  VelocityY    0.45096E+04      13   0.72770E-02   0.36165E-04 
c  VelocityZ    0.45096E+04      13   0.72770E-02   0.64438E-04 
c  TurbEner     0.44403E+01      23   0.43116E-03   0.16434E-06 
c  Dissip       0.83359E+00      21   0.17381E-02   0.79967E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -187.64           53660           26332           26817
v  Velocity[x]            0.27278          2.0848         0.90615          0.9082
v  Velocity[y]           -0.38434         0.73171      0.00041301      0.00023816
v  Velocity[z]           -0.42415         0.51203      -0.0013817      -0.0015526
v  TurbEner            0.00038114        0.015934       0.0020937       0.0021354
v  Dissip               5.175e-06        0.018513      0.00026482      0.00022661
v  TurbVisc              0.096842          11.013          3.4655          3.9186
v  total_pressure           83088      1.5571e+05      1.1877e+05      1.1953e+05


 TIME FOR THE TIME STEP               29:        0.11540E+00

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


 INSTANT    0.300000000E+02   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004760E+04
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 :  0.23184E+00 0.13176E+01
   Friction velocity        uet   :  0.14475E-01 0.82235E-01
   Friction velocity        uk    :  0.10693E-01 0.33204E-01
   Dimensionless distance   yplus :  0.25909E+03 0.81827E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71258E+01     149   0.17724E-02   0.22301E-01 
c  VelocityX    0.45183E+04      13   0.76756E-02   0.44264E-03 
c  VelocityY    0.45183E+04      13   0.76756E-02   0.33345E-04 
c  VelocityZ    0.45183E+04      13   0.76756E-02   0.67926E-04 
c  TurbEner     0.45066E+01      23   0.43403E-03   0.15859E-06 
c  Dissip       0.88341E+00      21   0.20899E-02   0.10730E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.35           53725           26365           26850
v  Velocity[x]            0.27363          2.1249         0.90634         0.90841
v  Velocity[y]           -0.39818         0.72389      0.00043249      0.00025978
v  Velocity[z]           -0.42811         0.51717      -0.0013968      -0.0015723
v  TurbEner             0.0004068        0.015951       0.0021475       0.0021894
v  Dissip              5.6004e-06        0.019477      0.00027374      0.00023418
v  TurbVisc               0.10117          11.013          3.5096          3.9642
v  total_pressure           83083      1.5578e+05       1.188e+05      1.1957e+05


 TIME FOR THE TIME STEP               30:        0.11668E+00

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


 INSTANT    0.310000000E+02   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004748E+04
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 :  0.23161E+00 0.12307E+01
   Friction velocity        uet   :  0.14397E-01 0.75181E-01
   Friction velocity        uk    :  0.11047E-01 0.33373E-01
   Dimensionless distance   yplus :  0.26748E+03 0.82245E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72213E+01     149   0.15245E-02   0.22723E-01 
c  VelocityX    0.45270E+04      13   0.68063E-02   0.42866E-03 
c  VelocityY    0.45270E+04      13   0.68063E-02   0.71071E-04 
c  VelocityZ    0.45270E+04      13   0.68063E-02   0.13522E-03 
c  TurbEner     0.45719E+01      23   0.43032E-03   0.15421E-06 
c  Dissip       0.94051E+00      21   0.22815E-02   0.12447E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.82           53815           26398           26883
v  Velocity[x]            0.27592          2.1655         0.90645         0.90852
v  Velocity[y]            -0.3814         0.73215      0.00046104      0.00027654
v  Velocity[z]           -0.43236         0.51237      -0.0014022      -0.0015777
v  TurbEner            0.00043243        0.016089       0.0022011       0.0022432
v  Dissip              6.0032e-06        0.020619      0.00028278      0.00024185
v  TurbVisc               0.10501          11.013          3.5546          4.0114
v  total_pressure           83089      1.5585e+05      1.1884e+05       1.196e+05


 TIME FOR THE TIME STEP               31:        0.11691E+00

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


 INSTANT    0.320000000E+02   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004476E+04
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 :  0.23218E+00 0.13227E+01
   Friction velocity        uet   :  0.14372E-01 0.81611E-01
   Friction velocity        uk    :  0.11390E-01 0.33488E-01
   Dimensionless distance   yplus :  0.27578E+03 0.82528E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64534E+01     149   0.15006E-02   0.20373E-01 
c  VelocityX    0.45352E+04      13   0.78715E-02   0.41269E-03 
c  VelocityY    0.45352E+04      13   0.78715E-02   0.35691E-04 
c  VelocityZ    0.45352E+04      13   0.78715E-02   0.50418E-04 
c  TurbEner     0.46361E+01      23   0.43206E-03   0.14850E-06 
c  Dissip       0.10010E+01      21   0.25355E-02   0.14277E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.99           53869           26430           26917
v  Velocity[x]            0.27604           2.178         0.90662         0.90868
v  Velocity[y]           -0.39573         0.72203      0.00046302       0.0002777
v  Velocity[z]           -0.43509         0.51907      -0.0014058      -0.0015812
v  TurbEner            0.00045771        0.016425       0.0022538       0.0022964
v  Dissip              6.4803e-06        0.022112      0.00029186      0.00024957
v  TurbVisc               0.10846          11.013          3.6004            4.06
v  total_pressure           83084      1.5591e+05      1.1887e+05      1.1963e+05


 TIME FOR THE TIME STEP               32:        0.11625E+00

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


 INSTANT    0.330000000E+02   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400005041E+04
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 :  0.23226E+00 0.12446E+01
   Friction velocity        uet   :  0.14320E-01 0.74866E-01
   Friction velocity        uk    :  0.11718E-01 0.33453E-01
   Dimensionless distance   yplus :  0.28374E+03 0.82441E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71778E+01     149   0.17532E-02   0.22763E-01 
c  VelocityX    0.45432E+04      13   0.67559E-02   0.54870E-03 
c  VelocityY    0.45432E+04      13   0.67559E-02   0.32384E-04 
c  VelocityZ    0.45432E+04      13   0.67559E-02   0.45847E-04 
c  TurbEner     0.46981E+01      23   0.44009E-03   0.14472E-06 
c  Dissip       0.10594E+01      20   0.32503E-02   0.18307E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -182.21           53919           26462           26949
v  Velocity[x]            0.27865           2.011         0.90675          0.9088
v  Velocity[y]            -0.3797         0.73082      0.00048534      0.00029403
v  Velocity[z]           -0.43588         0.51469      -0.0014178      -0.0015866
v  TurbEner             0.0004824        0.017167       0.0023059        0.002349
v  Dissip              7.0657e-06        0.024469      0.00030094      0.00025732
v  TurbVisc               0.11162          11.013          3.6463          4.1095
v  total_pressure           83090      1.5598e+05       1.189e+05      1.1966e+05


 TIME FOR THE TIME STEP               33:        0.11721E+00

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


 INSTANT    0.340000000E+02   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004880E+04
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 :  0.23200E+00 0.13261E+01
   Friction velocity        uet   :  0.14251E-01 0.81284E-01
   Friction velocity        uk    :  0.12030E-01 0.33563E-01
   Dimensionless distance   yplus :  0.29138E+03 0.82712E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60270E+01     148   0.13649E-02   0.19170E-01 
c  VelocityX    0.45506E+04      13   0.63607E-02   0.33635E-03 
c  VelocityY    0.45506E+04      13   0.63607E-02   0.30688E-04 
c  VelocityZ    0.45506E+04      13   0.63607E-02   0.53337E-04 
c  TurbEner     0.47553E+01      22   0.44339E-03   0.14153E-06 
c  Dissip       0.10751E+01      20   0.13018E-02   0.57639E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.35           53969           26491           26978
v  Velocity[x]            0.28032          2.0767         0.90686         0.90891
v  Velocity[y]           -0.39362         0.72103      0.00047855      0.00029115
v  Velocity[z]           -0.43721         0.52106      -0.0014191       -0.001586
v  TurbEner            0.00050665        0.016403       0.0023569       0.0024008
v  Dissip                 7.8e-06        0.024252      0.00030951       0.0002647
v  TurbVisc               0.11454          11.013          3.6925          4.1597
v  total_pressure           83084      1.5603e+05      1.1893e+05      1.1969e+05


 TIME FOR THE TIME STEP               34:        0.11726E+00

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


 INSTANT    0.350000000E+02   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004729E+04
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 :  0.23262E+00 0.12207E+01
   Friction velocity        uet   :  0.14241E-01 0.74587E-01
   Friction velocity        uk    :  0.12329E-01 0.33654E-01
   Dimensionless distance   yplus :  0.29871E+03 0.82937E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65309E+01     148   0.14650E-02   0.20841E-01 
c  VelocityX    0.45577E+04      13   0.71574E-02   0.33127E-03 
c  VelocityY    0.45577E+04      13   0.71574E-02   0.55522E-04 
c  VelocityZ    0.45577E+04      13   0.71574E-02   0.11957E-03 
c  TurbEner     0.48143E+01      22   0.41514E-03   0.13588E-06 
c  Dissip       0.11185E+01      20   0.15644E-02   0.70048E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.21           54044           26519           27007
v  Velocity[x]            0.28195          2.1258         0.90695         0.90901
v  Velocity[y]           -0.37623         0.72883       0.0005006      0.00030684
v  Velocity[z]           -0.43857         0.51527      -0.0014052        -0.00157
v  TurbEner            0.00053058        0.016288       0.0024074       0.0024521
v  Dissip              8.7303e-06        0.024946      0.00031814      0.00027212
v  TurbVisc               0.11734          11.013          3.7389          4.2105
v  total_pressure           83089      1.5609e+05      1.1896e+05      1.1972e+05


 TIME FOR THE TIME STEP               35:        0.11691E+00

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


 INSTANT    0.360000000E+02   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004623E+04
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 :  0.23343E+00 0.13296E+01
   Friction velocity        uet   :  0.14247E-01 0.80998E-01
   Friction velocity        uk    :  0.12616E-01 0.33568E-01
   Dimensionless distance   yplus :  0.30571E+03 0.82725E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62706E+01     147   0.15025E-02   0.20083E-01 
c  VelocityX    0.45643E+04      13   0.71185E-02   0.39266E-03 
c  VelocityY    0.45643E+04      13   0.71185E-02   0.38394E-04 
c  VelocityZ    0.45643E+04      13   0.71185E-02   0.69206E-04 
c  TurbEner     0.48725E+01      22   0.41076E-03   0.13291E-06 
c  Dissip       0.11719E+01      20   0.20316E-02   0.10813E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.83           54088           26547           27035
v  Velocity[x]            0.28283           2.159         0.90708         0.90911
v  Velocity[y]           -0.39162         0.71912      0.00048963      0.00030043
v  Velocity[z]           -0.43733         0.51902      -0.0014053      -0.0015633
v  TurbEner            0.00055447        0.016335       0.0024571       0.0025026
v  Dissip              9.9023e-06        0.025912      0.00032675      0.00027954
v  TurbVisc                0.1201          11.013          3.7853          4.2616
v  total_pressure           83083      1.5614e+05      1.1899e+05      1.1975e+05


 TIME FOR THE TIME STEP               36:        0.11701E+00

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


 INSTANT    0.370000000E+02   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004506E+04
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 :  0.23437E+00 0.12404E+01
   Friction velocity        uet   :  0.14265E-01 0.74270E-01
   Friction velocity        uk    :  0.12897E-01 0.33658E-01
   Dimensionless distance   yplus :  0.31253E+03 0.82946E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66342E+01     145   0.13544E-02   0.21286E-01 
c  VelocityX    0.45706E+04      13   0.73574E-02   0.43361E-03 
c  VelocityY    0.45706E+04      13   0.73574E-02   0.29416E-04 
c  VelocityZ    0.45706E+04      13   0.73574E-02   0.40916E-04 
c  TurbEner     0.49290E+01      22   0.39391E-03   0.12893E-06 
c  Dissip       0.12290E+01      20   0.20328E-02   0.99493E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.37           54136           26570           27059
v  Velocity[x]            0.28399          2.1858         0.90717          0.9092
v  Velocity[y]            -0.3763         0.72697      0.00049628      0.00030378
v  Velocity[z]           -0.43695         0.51134      -0.0014115      -0.0015645
v  TurbEner            0.00057823        0.016459       0.0025057       0.0025522
v  Dissip              1.1379e-05        0.027091      0.00033521      0.00028683
v  TurbVisc               0.12289          11.076          3.8316          4.3128
v  total_pressure           83089      1.5619e+05      1.1901e+05      1.1977e+05


 TIME FOR THE TIME STEP               37:        0.11909E+00

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


 INSTANT    0.380000000E+02   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004462E+04
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 :  0.23425E+00 0.13295E+01
   Friction velocity        uet   :  0.14223E-01 0.80582E-01
   Friction velocity        uk    :  0.13171E-01 0.33709E-01
   Dimensionless distance   yplus :  0.31911E+03 0.83074E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63831E+01     144   0.16203E-02   0.20530E-01 
c  VelocityX    0.45762E+04      13   0.75726E-02   0.45649E-03 
c  VelocityY    0.45762E+04      13   0.75726E-02   0.27722E-04 
c  VelocityZ    0.45762E+04      13   0.75726E-02   0.49389E-04 
c  TurbEner     0.49837E+01      22   0.39274E-03   0.12616E-06 
c  Dissip       0.12745E+01      19   0.28353E-02   0.13708E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.21           54172           26592           27082
v  Velocity[x]            0.28514          2.0118         0.90728          0.9093
v  Velocity[y]           -0.38934         0.71614      0.00049336      0.00030622
v  Velocity[z]            -0.4381         0.51844      -0.0014103      -0.0015591
v  TurbEner            0.00060212        0.017012       0.0025533       0.0026008
v  Dissip              1.3184e-05        0.029197      0.00034349      0.00029401
v  TurbVisc               0.12574          11.166          3.8777           4.364
v  total_pressure           83082      1.5623e+05      1.1903e+05       1.198e+05


 TIME FOR THE TIME STEP               38:        0.11831E+00

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


 INSTANT    0.390000000E+02   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004157E+04
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 :  0.23467E+00 0.12236E+01
   Friction velocity        uet   :  0.14217E-01 0.73992E-01
   Friction velocity        uk    :  0.13440E-01 0.33641E-01
   Dimensionless distance   yplus :  0.32556E+03 0.82904E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67784E+01     144   0.16485E-02   0.21864E-01 
c  VelocityX    0.45816E+04      13   0.66227E-02   0.36585E-03 
c  VelocityY    0.45816E+04      13   0.66227E-02   0.60506E-04 
c  VelocityZ    0.45816E+04      13   0.66227E-02   0.13229E-03 
c  TurbEner     0.50355E+01      22   0.39587E-03   0.12444E-06 
c  Dissip       0.12765E+01      19   0.15190E-02   0.66670E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.49           54218           26612           27102
v  Velocity[x]            0.28666          2.0851         0.90734         0.90935
v  Velocity[y]           -0.37411         0.72308      0.00051187      0.00032313
v  Velocity[z]           -0.43654         0.51303      -0.0013971      -0.0015409
v  TurbEner            0.00062606        0.016296       0.0025996       0.0026482
v  Dissip              1.5358e-05        0.028597      0.00035114      0.00030073
v  TurbVisc               0.12869          11.193          3.9234          4.4148
v  total_pressure           83087      1.5627e+05      1.1905e+05      1.1982e+05


 TIME FOR THE TIME STEP               39:        0.11854E+00

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


 INSTANT    0.400000000E+02   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400004439E+04
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 :  0.23540E+00 0.13307E+01
   Friction velocity        uet   :  0.14234E-01 0.80309E-01
   Friction velocity        uk    :  0.13705E-01 0.33721E-01
   Dimensionless distance   yplus :  0.33189E+03 0.83103E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63032E+01     142   0.13196E-02   0.20375E-01 
c  VelocityX    0.45864E+04      13   0.65221E-02   0.37844E-03 
c  VelocityY    0.45864E+04      13   0.65221E-02   0.37086E-04 
c  VelocityZ    0.45864E+04      13   0.65221E-02   0.60661E-04 
c  TurbEner     0.50870E+01      22   0.35362E-03   0.11896E-06 
c  Dissip       0.13085E+01      19   0.12126E-02   0.51699E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -171.7           54248           26633           27123
v  Velocity[x]            0.28713          2.1331          0.9074          0.9094
v  Velocity[y]           -0.38848          0.7128      0.00050335      0.00031547
v  Velocity[z]            -0.4362         0.51922      -0.0014022      -0.0015448
v  TurbEner            0.00064895        0.016106       0.0026447       0.0026944
v  Dissip              1.7925e-05        0.028927      0.00035872      0.00030736
v  TurbVisc               0.13155          11.242          3.9686           4.465
v  total_pressure           83082      1.5631e+05      1.1907e+05      1.1984e+05


 TIME FOR THE TIME STEP               40:        0.11840E+00

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


 INSTANT    0.410000000E+02   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400003924E+04
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 :  0.23555E+00 0.12268E+01
   Friction velocity        uet   :  0.14220E-01 0.73690E-01
   Friction velocity        uk    :  0.13953E-01 0.33807E-01
   Dimensionless distance   yplus :  0.33822E+03 0.83315E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56681E+01     120   0.13390E-02   0.18336E-01 
c  VelocityX    0.45909E+04      13   0.71524E-02   0.32466E-03 
c  VelocityY    0.45909E+04      13   0.71524E-02   0.26460E-04 
c  VelocityZ    0.45909E+04      13   0.71524E-02   0.34974E-04 
c  TurbEner     0.51386E+01      22   0.32649E-03   0.11447E-06 
c  Dissip       0.13521E+01      19   0.15302E-02   0.69503E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -182.51           54280           26649           27140
v  Velocity[x]            0.28829          2.1722         0.90749         0.90947
v  Velocity[y]           -0.37145         0.72103       0.0005145       0.0003244
v  Velocity[z]           -0.43489         0.51294      -0.0013977      -0.0015341
v  TurbEner            0.00067365        0.016057       0.0026884       0.0027392
v  Dissip              2.0887e-05        0.029571      0.00036617      0.00031386
v  TurbVisc               0.13441           11.25          4.0132          4.5145
v  total_pressure           83085      1.5634e+05      1.1909e+05      1.1985e+05


 TIME FOR THE TIME STEP               41:        0.11232E+00

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


 INSTANT    0.420000000E+02   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002956E+04
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 :  0.23561E+00 0.13295E+01
   Friction velocity        uet   :  0.14202E-01 0.79990E-01
   Friction velocity        uk    :  0.14216E-01 0.33696E-01
   Dimensionless distance   yplus :  0.34463E+03 0.83039E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62398E+01     118   0.15716E-02   0.20245E-01 
c  VelocityX    0.45950E+04      13   0.76403E-02   0.40300E-03 
c  VelocityY    0.45950E+04      13   0.76403E-02   0.26521E-04 
c  VelocityZ    0.45950E+04      13   0.76403E-02   0.52758E-04 
c  TurbEner     0.51885E+01      22   0.31999E-03   0.11121E-06 
c  Dissip       0.13846E+01      19   0.24052E-02   0.96607E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.43           54295           26665           27157
v  Velocity[x]            0.28879          2.0059         0.90756         0.90953
v  Velocity[y]           -0.38717         0.70975      0.00051234      0.00032696
v  Velocity[z]           -0.43371         0.51665      -0.0014019      -0.0015351
v  TurbEner            0.00069769        0.016506        0.002731       0.0027828
v  Dissip              2.4132e-05        0.031338      0.00037341      0.00032022
v  TurbVisc               0.13751          11.251          4.0567          4.5628
v  total_pressure           83080      1.5637e+05      1.1911e+05      1.1987e+05


 TIME FOR THE TIME STEP               42:        0.11273E+00

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


 INSTANT    0.430000000E+02   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400003658E+04
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 :  0.23624E+00 0.12305E+01
   Friction velocity        uet   :  0.14222E-01 0.73639E-01
   Friction velocity        uk    :  0.14467E-01 0.33781E-01
   Dimensionless distance   yplus :  0.35107E+03 0.83250E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75013E+01     113   0.14298E-02   0.24345E-01 
c  VelocityX    0.45987E+04      13   0.69451E-02   0.45664E-03 
c  VelocityY    0.45987E+04      13   0.69451E-02   0.47825E-04 
c  VelocityZ    0.45987E+04      13   0.69451E-02   0.12914E-03 
c  TurbEner     0.52345E+01      21   0.33279E-03   0.10848E-06 
c  Dissip       0.13707E+01      19   0.20289E-02   0.86413E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.13           54351           26679           27171
v  Velocity[x]            0.28945          2.0864         0.90758         0.90954
v  Velocity[y]           -0.37205         0.71311      0.00053332      0.00034094
v  Velocity[z]           -0.43278         0.50908      -0.0013918      -0.0015235
v  TurbEner            0.00072343        0.015751       0.0027715       0.0028244
v  Dissip              2.7726e-05        0.030178      0.00037987      0.00032597
v  TurbVisc               0.14063          11.298          4.0993            4.61
v  total_pressure           83086      1.5639e+05      1.1912e+05      1.1989e+05


 TIME FOR THE TIME STEP               43:        0.11235E+00

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


 INSTANT    0.440000000E+02   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400003349E+04
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 :  0.23624E+00 0.13319E+01
   Friction velocity        uet   :  0.14207E-01 0.79903E-01
   Friction velocity        uk    :  0.14732E-01 0.33863E-01
   Dimensionless distance   yplus :  0.35757E+03 0.83453E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71064E+01     111   0.15085E-02   0.23100E-01 
c  VelocityX    0.46020E+04      13   0.66664E-02   0.39551E-03 
c  VelocityY    0.46020E+04      13   0.66664E-02   0.64608E-04 
c  VelocityZ    0.46020E+04      13   0.66664E-02   0.62367E-04 
c  TurbEner     0.52813E+01      21   0.27831E-03   0.10196E-06 
c  Dissip       0.13804E+01      18   0.98959E-03   0.37201E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.17           54355           26693           27184
v  Velocity[x]             0.2899          2.1284         0.90766          0.9096
v  Velocity[y]           -0.38594         0.70634      0.00051558      0.00032754
v  Velocity[z]           -0.43218           0.516      -0.0013946       -0.001522
v  TurbEner            0.00074908        0.015544       0.0028107       0.0028645
v  Dissip               3.165e-05        0.029997      0.00038619      0.00033158
v  TurbVisc               0.14395          11.289          4.1405          4.6555
v  total_pressure           83080      1.5642e+05      1.1913e+05       1.199e+05


 TIME FOR THE TIME STEP               44:        0.11051E+00

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


 INSTANT    0.450000000E+02   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400003239E+04
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 :  0.23646E+00 0.12378E+01
   Friction velocity        uet   :  0.14208E-01 0.73158E-01
   Friction velocity        uk    :  0.14991E-01 0.33874E-01
   Dimensionless distance   yplus :  0.36414E+03 0.83479E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70343E+01     111   0.16008E-02   0.22901E-01 
c  VelocityX    0.46052E+04      13   0.69314E-02   0.37359E-03 
c  VelocityY    0.46052E+04      13   0.69314E-02   0.45193E-04 
c  VelocityZ    0.46052E+04      13   0.69314E-02   0.32015E-04 
c  TurbEner     0.53285E+01      21   0.25221E-03   0.96454E-07 
c  Dissip       0.14129E+01      18   0.11437E-02   0.44256E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -183.05           54379           26703           27195
v  Velocity[x]            0.29083          2.1747         0.90771         0.90963
v  Velocity[y]            -0.3712         0.71558      0.00053783      0.00034497
v  Velocity[z]            -0.4307         0.51046       -0.001387      -0.0015101
v  TurbEner            0.00077337        0.015555       0.0028484        0.002903
v  Dissip              3.5753e-05        0.030374       0.0003924      0.00033707
v  TurbVisc               0.14727          11.297          4.1804          4.6996
v  total_pressure           83084      1.5644e+05      1.1914e+05      1.1991e+05


 TIME FOR THE TIME STEP               45:        0.10887E+00

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


 INSTANT    0.460000000E+02   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400003452E+04
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 :  0.23680E+00 0.13273E+01
   Friction velocity        uet   :  0.14218E-01 0.79480E-01
   Friction velocity        uk    :  0.15232E-01 0.33901E-01
   Dimensionless distance   yplus :  0.37055E+03 0.84105E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66885E+01     108   0.14507E-02   0.21788E-01 
c  VelocityX    0.46078E+04      13   0.70042E-02   0.43987E-03 
c  VelocityY    0.46078E+04      13   0.70042E-02   0.39907E-04 
c  VelocityZ    0.46078E+04      13   0.70042E-02   0.47189E-04 
c  TurbEner     0.53723E+01      21   0.25193E-03   0.91237E-07 
c  Dissip       0.14342E+01      18   0.21635E-02   0.73296E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.05           54386           26713           27206
v  Velocity[x]            0.29086          2.0049         0.90775         0.90967
v  Velocity[y]           -0.38549         0.70304      0.00053715      0.00034607
v  Velocity[z]           -0.42839          0.5169       -0.001399      -0.0015249
v  TurbEner            0.00080173        0.016063       0.0028842       0.0029397
v  Dissip              3.9957e-05         0.03196      0.00039827      0.00034227
v  TurbVisc               0.15049          11.343          4.2188          4.7419
v  total_pressure           83079      1.5646e+05      1.1915e+05      1.1992e+05


 TIME FOR THE TIME STEP               46:        0.10825E+00

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


 INSTANT    0.470000000E+02   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002924E+04
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 :  0.23649E+00 0.12597E+01
   Friction velocity        uet   :  0.14190E-01 0.73402E-01
   Friction velocity        uk    :  0.15509E-01 0.34124E-01
   Dimensionless distance   yplus :  0.37715E+03 0.85309E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65898E+01     106   0.13650E-02   0.21478E-01 
c  VelocityX    0.46103E+04      13   0.66879E-02   0.33111E-03 
c  VelocityY    0.46103E+04      13   0.66879E-02   0.27245E-04 
c  VelocityZ    0.46103E+04      13   0.66879E-02   0.10618E-03 
c  TurbEner     0.54141E+01      21   0.25967E-03   0.86748E-07 
c  Dissip       0.14130E+01      18   0.20991E-02   0.85451E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.14           54421           26721           27214
v  Velocity[x]            0.29155          2.0869         0.90778         0.90968
v  Velocity[y]           -0.36877         0.70661      0.00054698      0.00035148
v  Velocity[z]           -0.42648         0.51062       -0.001384      -0.0015068
v  TurbEner            0.00082728        0.015419        0.002918       0.0029743
v  Dissip              4.4391e-05        0.030751      0.00040342      0.00034691
v  TurbVisc               0.15398          11.334          4.2556          4.7823
v  total_pressure           83084      1.5647e+05      1.1916e+05      1.1993e+05


 TIME FOR THE TIME STEP               47:        0.10816E+00

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


 INSTANT    0.480000000E+02   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002684E+04
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 :  0.23666E+00 0.13294E+01
   Friction velocity        uet   :  0.14193E-01 0.79482E-01
   Friction velocity        uk    :  0.15754E-01 0.34559E-01
   Dimensionless distance   yplus :  0.38355E+03 0.86396E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62010E+01     106   0.13890E-02   0.20237E-01 
c  VelocityX    0.46125E+04      13   0.66922E-02   0.34881E-03 
c  VelocityY    0.46125E+04      13   0.66922E-02   0.27514E-04 
c  VelocityZ    0.46125E+04      13   0.66922E-02   0.50253E-04 
c  TurbEner     0.54557E+01      21   0.20399E-03   0.79075E-07 
c  Dissip       0.14214E+01      18   0.86363E-03   0.26764E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.34           54451           26730           27222
v  Velocity[x]            0.29147          2.1369         0.90782         0.90971
v  Velocity[y]           -0.38464         0.70074      0.00053494      0.00034271
v  Velocity[z]           -0.42429         0.51439      -0.0013904      -0.0015125
v  TurbEner             0.0008551        0.015222       0.0029501       0.0030071
v  Dissip              4.8974e-05        0.030483      0.00040842      0.00035139
v  TurbVisc               0.15728          11.341          4.2906          4.8208
v  total_pressure           83078      1.5649e+05      1.1917e+05      1.1994e+05


 TIME FOR THE TIME STEP               48:        0.10764E+00

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


 INSTANT    0.490000000E+02   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002547E+04
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 :  0.23727E+00 0.12181E+01
   Friction velocity        uet   :  0.14224E-01 0.72791E-01
   Friction velocity        uk    :  0.16017E-01 0.34965E-01
   Dimensionless distance   yplus :  0.39002E+03 0.87409E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61719E+01      93   0.12372E-02   0.20147E-01 
c  VelocityX    0.46145E+04      13   0.75235E-02   0.35949E-03 
c  VelocityY    0.46145E+04      13   0.75235E-02   0.26766E-04 
c  VelocityZ    0.46145E+04      13   0.75235E-02   0.32142E-04 
c  TurbEner     0.54961E+01      20   0.18248E-03   0.72756E-07 
c  Dissip       0.14482E+01      18   0.97417E-03   0.32417E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -182.98           54472           26736           27228
v  Velocity[x]            0.29156          2.1776         0.90785         0.90971
v  Velocity[y]           -0.36998         0.70832      0.00054414      0.00034774
v  Velocity[z]           -0.42403         0.50675      -0.0013877      -0.0015063
v  TurbEner            0.00088093        0.015243       0.0029803       0.0030379
v  Dissip              5.3667e-05        0.030748      0.00041319      0.00035563
v  TurbVisc               0.16067          11.319           4.324          4.8574
v  total_pressure           83084       1.565e+05      1.1918e+05      1.1994e+05


 TIME FOR THE TIME STEP               49:        0.10482E+00

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


 INSTANT    0.500000000E+02   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001038E+04
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 :  0.23767E+00 0.13285E+01
   Friction velocity        uet   :  0.14243E-01 0.79353E-01
   Friction velocity        uk    :  0.16257E-01 0.35353E-01
   Dimensionless distance   yplus :  0.39617E+03 0.88381E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.74106E+01      93   0.16722E-02   0.24194E-01 
c  VelocityX    0.46162E+04      13   0.75478E-02   0.46904E-03 
c  VelocityY    0.46162E+04      13   0.75478E-02   0.43543E-04 
c  VelocityZ    0.46162E+04      13   0.75478E-02   0.39381E-04 
c  TurbEner     0.55346E+01      20   0.19163E-03   0.67091E-07 
c  Dissip       0.14660E+01      18   0.20388E-02   0.59034E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.4           54476           26742           27236
v  Velocity[x]             0.2923          2.0049         0.90791         0.90978
v  Velocity[y]           -0.38447         0.69837      0.00054247      0.00035173
v  Velocity[z]            -0.4257         0.51363      -0.0013861      -0.0015028
v  TurbEner            0.00090874        0.015767       0.0030089       0.0030669
v  Dissip               5.844e-05        0.032272      0.00041769      0.00035964
v  TurbVisc               0.16385          11.312          4.3555          4.8918
v  total_pressure           83079      1.5651e+05      1.1918e+05      1.1995e+05


 TIME FOR THE TIME STEP               50:        0.10460E+00

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


 INSTANT    0.510000000E+02   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000478E+04
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 :  0.23756E+00 0.12345E+01
   Friction velocity        uet   :  0.14234E-01 0.72747E-01
   Friction velocity        uk    :  0.16511E-01 0.35724E-01
   Dimensionless distance   yplus :  0.40244E+03 0.89309E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66387E+01      85   0.15985E-02   0.21716E-01 
c  VelocityX    0.46179E+04      13   0.72781E-02   0.38043E-03 
c  VelocityY    0.46179E+04      13   0.72781E-02   0.49481E-04 
c  VelocityZ    0.46179E+04      13   0.72781E-02   0.66609E-04 
c  TurbEner     0.55701E+01      20   0.20872E-03   0.62904E-07 
c  Dissip       0.14400E+01      18   0.21624E-02   0.81645E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -183.19           54463           26747           27240
v  Velocity[x]            0.29236          2.0872         0.90791         0.90976
v  Velocity[y]           -0.36923         0.70594      0.00056125      0.00036468
v  Velocity[z]           -0.42572         0.50888       -0.001375      -0.0014889
v  TurbEner            0.00093208        0.015146       0.0030354       0.0030939
v  Dissip              6.3272e-05        0.030963      0.00042146      0.00036309
v  TurbVisc               0.16705          11.341          4.3853          4.9243
v  total_pressure           83083      1.5652e+05      1.1919e+05      1.1996e+05


 TIME FOR THE TIME STEP               51:        0.10375E+00

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


 INSTANT    0.520000000E+02   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000473E+04
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 :  0.23806E+00 0.13280E+01
   Friction velocity        uet   :  0.14260E-01 0.79276E-01
   Friction velocity        uk    :  0.16722E-01 0.36067E-01
   Dimensionless distance   yplus :  0.40814E+03 0.90164E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65805E+01      86   0.13375E-02   0.21514E-01 
c  VelocityX    0.46192E+04      13   0.71029E-02   0.40915E-03 
c  VelocityY    0.46192E+04      13   0.71029E-02   0.35427E-04 
c  VelocityZ    0.46192E+04      13   0.71029E-02   0.42442E-04 
c  TurbEner     0.56040E+01      20   0.14805E-03   0.55077E-07 
c  Dissip       0.14463E+01      17   0.72144E-03   0.17247E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.01           54480           26752           27246
v  Velocity[x]            0.29208          2.1356         0.90795         0.90979
v  Velocity[y]           -0.38383         0.69657      0.00055756      0.00036123
v  Velocity[z]           -0.42643         0.51529      -0.0013724      -0.0014875
v  TurbEner            0.00095432         0.01499         0.00306        0.003119
v  Dissip              6.8082e-05        0.030665      0.00042501      0.00036629
v  TurbVisc               0.17017          11.388          4.4134          4.9548
v  total_pressure           83078      1.5653e+05      1.1919e+05      1.1996e+05


 TIME FOR THE TIME STEP               52:        0.10354E+00

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


 INSTANT    0.530000000E+02   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000764E+04
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 :  0.23767E+00 0.12655E+01
   Friction velocity        uet   :  0.14235E-01 0.73803E-01
   Friction velocity        uk    :  0.16920E-01 0.36386E-01
   Dimensionless distance   yplus :  0.41298E+03 0.90963E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61735E+01      82   0.12651E-02   0.20189E-01 
c  VelocityX    0.46206E+04      13   0.77040E-02   0.37312E-03 
c  VelocityY    0.46206E+04      13   0.77040E-02   0.29929E-04 
c  VelocityZ    0.46206E+04      13   0.77040E-02   0.34265E-04 
c  TurbEner     0.56376E+01      20   0.13801E-03   0.49075E-07 
c  Dissip       0.14743E+01      17   0.87001E-03   0.24255E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -181.23           54495           26755           27248
v  Velocity[x]            0.29266          2.1818         0.90794         0.90978
v  Velocity[y]           -0.36742         0.70452      0.00056315       0.0003625
v  Velocity[z]           -0.42699         0.50914      -0.0013646      -0.0014804
v  TurbEner            0.00097462         0.01504        0.003083       0.0031422
v  Dissip              7.2853e-05        0.030905      0.00042848      0.00036938
v  TurbVisc               0.17312           11.37          4.4396          4.9834
v  total_pressure           83083      1.5653e+05       1.192e+05      1.1996e+05


 TIME FOR THE TIME STEP               53:        0.10263E+00

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


 INSTANT    0.540000000E+02   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001029E+04
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 :  0.23752E+00 0.13266E+01
   Friction velocity        uet   :  0.14224E-01 0.79159E-01
   Friction velocity        uk    :  0.17099E-01 0.36690E-01
   Dimensionless distance   yplus :  0.41749E+03 0.91723E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.76093E+01      83   0.17493E-02   0.24916E-01 
c  VelocityX    0.46215E+04      13   0.71318E-02   0.42265E-03 
c  VelocityY    0.46215E+04      13   0.71318E-02   0.27023E-04 
c  VelocityZ    0.46215E+04      13   0.71318E-02   0.10763E-03 
c  TurbEner     0.56688E+01      19   0.15274E-03   0.43695E-07 
c  Dissip       0.14890E+01      17   0.17999E-02   0.43612E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.83           54511           26759           27253
v  Velocity[x]            0.29227          2.0233         0.90796         0.90979
v  Velocity[y]           -0.38349         0.69599      0.00056196      0.00036279
v  Velocity[z]           -0.42514          0.5131      -0.0013626      -0.0014814
v  TurbEner            0.00099349         0.01555       0.0031041       0.0031637
v  Dissip              7.7587e-05        0.032267      0.00043164      0.00037222
v  TurbVisc               0.17564          11.374          4.4642            5.01
v  total_pressure           83078      1.5654e+05       1.192e+05      1.1997e+05


 TIME FOR THE TIME STEP               54:        0.10244E+00

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


 INSTANT    0.550000000E+02   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999793E+04
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 :  0.23789E+00 0.12359E+01
   Friction velocity        uet   :  0.14245E-01 0.72537E-01
   Friction velocity        uk    :  0.17264E-01 0.36950E-01
   Dimensionless distance   yplus :  0.42166E+03 0.92372E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62083E+01      80   0.14048E-02   0.20334E-01 
c  VelocityX    0.46225E+04      13   0.63070E-02   0.31780E-03 
c  VelocityY    0.46225E+04      13   0.63070E-02   0.40874E-04 
c  VelocityZ    0.46225E+04      13   0.63070E-02   0.63020E-04 
c  TurbEner     0.56962E+01      19   0.16786E-03   0.39672E-07 
c  Dissip       0.14573E+01      17   0.21714E-02   0.77713E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -183.29           54525           26762           27256
v  Velocity[x]            0.29248          2.0919         0.90797         0.90979
v  Velocity[y]           -0.36896         0.70466      0.00057617      0.00037169
v  Velocity[z]           -0.42565         0.50561      -0.0013528      -0.0014698
v  TurbEner             0.0010101        0.014981       0.0031232       0.0031831
v  Dissip              8.2252e-05         0.03094      0.00043404      0.00037445
v  TurbVisc               0.17622          11.348           4.487          5.0348
v  total_pressure           83084      1.5654e+05       1.192e+05      1.1997e+05


 TIME FOR THE TIME STEP               55:        0.10184E+00

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


 INSTANT    0.560000000E+02   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999779E+04
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 :  0.23744E+00 0.13266E+01
   Friction velocity        uet   :  0.14216E-01 0.79138E-01
   Friction velocity        uk    :  0.17408E-01 0.37185E-01
   Dimensionless distance   yplus :  0.42550E+03 0.92960E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59575E+01      81   0.15227E-02   0.19498E-01 
c  VelocityX    0.46234E+04      13   0.74496E-02   0.31475E-03 
c  VelocityY    0.46234E+04      13   0.74496E-02   0.36277E-04 
c  VelocityZ    0.46234E+04      13   0.74496E-02   0.41808E-04 
c  TurbEner     0.57233E+01      19   0.10760E-03   0.33356E-07 
c  Dissip       0.14610E+01      16   0.60760E-03   0.10244E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -171.2           54519           26764           27258
v  Velocity[x]            0.29321          2.1522         0.90799         0.90982
v  Velocity[y]           -0.38318         0.69168      0.00057728      0.00037432
v  Velocity[z]           -0.42597         0.51301       -0.001346      -0.0014662
v  TurbEner              0.001024        0.014831       0.0031408        0.003201
v  Dissip              8.6805e-05        0.030631      0.00043636      0.00037656
v  TurbVisc               0.17516          11.349          4.5082          5.0576
v  total_pressure           83077      1.5655e+05       1.192e+05      1.1997e+05


 TIME FOR THE TIME STEP               56:        0.10205E+00

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


 INSTANT    0.570000000E+02   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000343E+04
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 :  0.23727E+00 0.12189E+01
   Friction velocity        uet   :  0.14205E-01 0.72700E-01
   Friction velocity        uk    :  0.17527E-01 0.37355E-01
   Dimensionless distance   yplus :  0.42895E+03 0.93384E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62392E+01      77   0.14665E-02   0.20440E-01 
c  VelocityX    0.46243E+04      12   0.69148E-02   0.42395E-03 
c  VelocityY    0.46243E+04      12   0.69148E-02   0.25815E-04 
c  VelocityZ    0.46243E+04      12   0.69148E-02   0.36159E-04 
c  TurbEner     0.57492E+01      19   0.10395E-03   0.29560E-07 
c  Dissip       0.14900E+01      16   0.91113E-03   0.21991E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -180.86           54500           26766           27260
v  Velocity[x]            0.29265          2.1883         0.90801         0.90982
v  Velocity[y]           -0.36872         0.70195      0.00058768      0.00038036
v  Velocity[z]            -0.4256         0.50776      -0.0013384      -0.0014524
v  TurbEner             0.0010387        0.014934       0.0031568       0.0032172
v  Dissip              9.1224e-05        0.031014      0.00043863      0.00037859
v  TurbVisc               0.17406          11.324          4.5278          5.0788
v  total_pressure           83082      1.5655e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               57:        0.99919E-01

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


 INSTANT    0.580000000E+02   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999673E+04
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 :  0.23768E+00 0.13242E+01
   Friction velocity        uet   :  0.14228E-01 0.78978E-01
   Friction velocity        uk    :  0.17652E-01 0.37501E-01
   Dimensionless distance   yplus :  0.43211E+03 0.93750E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57347E+01      71   0.13172E-02   0.18778E-01 
c  VelocityX    0.46248E+04      12   0.69430E-02   0.40305E-03 
c  VelocityY    0.46248E+04      12   0.69430E-02   0.30251E-04 
c  VelocityZ    0.46248E+04      12   0.69430E-02   0.30439E-04 
c  TurbEner     0.57722E+01      18   0.13629E-03   0.25942E-07 
c  Dissip       0.15068E+01      16   0.21018E-02   0.54806E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.03           54510           26769           27263
v  Velocity[x]            0.29241          2.0167           0.908         0.90982
v  Velocity[y]           -0.38347         0.69632      0.00058097      0.00037591
v  Velocity[z]            -0.4256         0.51426      -0.0013459      -0.0014607
v  TurbEner             0.0010508        0.015485       0.0031715        0.003232
v  Dissip              9.2143e-05        0.032623      0.00044065      0.00038039
v  TurbVisc               0.17283           11.32          4.5459          5.0983
v  total_pressure           83078      1.5656e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               58:        0.99318E-01

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


 INSTANT    0.590000000E+02   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999456E+04
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 :  0.23767E+00 0.12142E+01
   Friction velocity        uet   :  0.14226E-01 0.72410E-01
   Friction velocity        uk    :  0.17755E-01 0.37639E-01
   Dimensionless distance   yplus :  0.43496E+03 0.94096E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63187E+01      69   0.13890E-02   0.20689E-01 
c  VelocityX    0.46254E+04      12   0.67221E-02   0.36308E-03 
c  VelocityY    0.46254E+04      12   0.67221E-02   0.32272E-04 
c  VelocityZ    0.46254E+04      12   0.67221E-02   0.59782E-04 
c  TurbEner     0.57923E+01      18   0.15250E-03   0.22996E-07 
c  Dissip       0.14813E+01      17   0.19810E-02   0.63399E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.12           54521           26769           27263
v  Velocity[x]            0.29312          2.0946         0.90798         0.90979
v  Velocity[y]           -0.36706         0.70363      0.00058443      0.00037662
v  Velocity[z]           -0.42476         0.50829      -0.0013398      -0.0014565
v  TurbEner             0.0010584        0.014919       0.0031845       0.0032451
v  Dissip              9.2119e-05        0.031413      0.00044205       0.0003817
v  TurbVisc               0.17164          11.348          4.5626          5.1163
v  total_pressure           83082      1.5656e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               59:        0.98036E-01

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


 INSTANT    0.600000000E+02   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999580E+04
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 :  0.23725E+00 0.13262E+01
   Friction velocity        uet   :  0.14200E-01 0.79078E-01
   Friction velocity        uk    :  0.17819E-01 0.37786E-01
   Dimensionless distance   yplus :  0.43751E+03 0.94435E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54345E+01      58   0.11800E-02   0.17809E-01 
c  VelocityX    0.46260E+04      13   0.60939E-02   0.29562E-03 
c  VelocityY    0.46260E+04      13   0.60939E-02   0.26818E-04 
c  VelocityZ    0.46260E+04      13   0.60939E-02   0.90483E-04 
c  TurbEner     0.58120E+01      18   0.91713E-04   0.18532E-07 
c  Dissip       0.14892E+01      15   0.57813E-03   0.70146E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.43           54532           26771           27265
v  Velocity[x]            0.29296          2.1477           0.908         0.90981
v  Velocity[y]           -0.38312         0.69469       0.0005842      0.00037741
v  Velocity[z]            -0.4238         0.51227      -0.0013317      -0.0014495
v  TurbEner              0.001048        0.014775       0.0031963        0.003257
v  Dissip              9.2117e-05        0.031095      0.00044343      0.00038296
v  TurbVisc               0.17127           11.33          4.5779          5.1327
v  total_pressure           83077      1.5656e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               60:        0.96984E-01

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


 INSTANT    0.610000000E+02   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997639E+04
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 :  0.23796E+00 0.12273E+01
   Friction velocity        uet   :  0.14241E-01 0.72512E-01
   Friction velocity        uk    :  0.17731E-01 0.37932E-01
   Dimensionless distance   yplus :  0.43650E+03 0.94668E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55142E+01      54   0.11466E-02   0.18074E-01 
c  VelocityX    0.46265E+04      12   0.70335E-02   0.30861E-03 
c  VelocityY    0.46265E+04      12   0.70335E-02   0.23039E-04 
c  VelocityZ    0.46265E+04      12   0.70335E-02   0.39959E-04 
c  TurbEner     0.58306E+01      18   0.87828E-04   0.15688E-07 
c  Dissip       0.15138E+01      16   0.92079E-03   0.18532E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.53           54541           26772           27266
v  Velocity[x]            0.29267          2.1836         0.90801         0.90982
v  Velocity[y]           -0.36847         0.70173      0.00059344      0.00037871
v  Velocity[z]           -0.42444         0.50498      -0.0013286      -0.0014473
v  TurbEner             0.0010449         0.01492        0.003207       0.0032677
v  Dissip              9.2126e-05        0.031567      0.00044483       0.0003842
v  TurbVisc               0.16991          11.338          4.5919          5.1477
v  total_pressure           83084      1.5656e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               61:        0.94987E-01

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


 INSTANT    0.620000000E+02   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000026E+04
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 :  0.23761E+00 0.13240E+01
   Friction velocity        uet   :  0.14219E-01 0.78929E-01
   Friction velocity        uk    :  0.17705E-01 0.37945E-01
   Dimensionless distance   yplus :  0.43503E+03 0.94859E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58573E+01      55   0.11741E-02   0.19186E-01 
c  VelocityX    0.46268E+04      12   0.72335E-02   0.32080E-03 
c  VelocityY    0.46268E+04      12   0.72335E-02   0.24543E-04 
c  VelocityZ    0.46268E+04      12   0.72335E-02   0.45822E-04 
c  TurbEner     0.58481E+01      17   0.85766E-04   0.13254E-07 
c  Dissip       0.15450E+01      16   0.10593E-02   0.22217E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.03           54548           26773           27267
v  Velocity[x]            0.29304          2.2046         0.90803         0.90983
v  Velocity[y]           -0.38349         0.69376      0.00058229      0.00036996
v  Velocity[z]           -0.42517         0.51194      -0.0013258      -0.0014413
v  TurbEner             0.0010399        0.015089       0.0032167       0.0032774
v  Dissip              9.2107e-05        0.032194       0.0004462      0.00038538
v  TurbVisc               0.16918          11.376          4.6047          5.1614
v  total_pressure           83077      1.5656e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               62:        0.95806E-01

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


 INSTANT    0.630000000E+02   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998961E+04
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 :  0.23756E+00 0.12160E+01
   Friction velocity        uet   :  0.14214E-01 0.72495E-01
   Friction velocity        uk    :  0.17663E-01 0.38082E-01
   Dimensionless distance   yplus :  0.43444E+03 0.95081E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67384E+01      56   0.15145E-02   0.22074E-01 
c  VelocityX    0.46272E+04      12   0.69571E-02   0.39297E-03 
c  VelocityY    0.46272E+04      12   0.69571E-02   0.38109E-04 
c  VelocityZ    0.46272E+04      12   0.69571E-02   0.49624E-04 
c  TurbEner     0.58639E+01      17   0.13576E-03   0.11573E-07 
c  Dissip       0.15694E+01      16   0.23471E-02   0.61198E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.69           54538           26772           27266
v  Velocity[x]            0.29258          2.0362         0.90803         0.90982
v  Velocity[y]           -0.36837         0.70083       0.0006006      0.00038366
v  Velocity[z]           -0.42522         0.50745       -0.001331      -0.0014478
v  TurbEner             0.0010323        0.015719       0.0032254       0.0032861
v  Dissip              9.2126e-05        0.034071      0.00044748      0.00038649
v  TurbVisc               0.16878          11.356          4.6164          5.1739
v  total_pressure           83082      1.5656e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               63:        0.95692E-01

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


 INSTANT    0.640000000E+02   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002025E+04
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 :  0.23780E+00 0.13247E+01
   Friction velocity        uet   :  0.14227E-01 0.78969E-01
   Friction velocity        uk    :  0.17598E-01 0.38257E-01
   Dimensionless distance   yplus :  0.43321E+03 0.95225E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73022E+01      64   0.16794E-02   0.23947E-01 
c  VelocityX    0.46275E+04      13   0.72191E-02   0.41581E-03 
c  VelocityY    0.46275E+04      13   0.72191E-02   0.53111E-04 
c  VelocityZ    0.46275E+04      13   0.72191E-02   0.48385E-04 
c  TurbEner     0.58764E+01      17   0.15263E-03   0.10852E-07 
c  Dissip       0.15363E+01      16   0.21995E-02   0.67968E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.84           54512           26774           27268
v  Velocity[x]             0.2925          2.1003         0.90805         0.90984
v  Velocity[y]           -0.38305         0.69411      0.00059005      0.00037816
v  Velocity[z]           -0.42401         0.51412      -0.0013207      -0.0014366
v  TurbEner             0.0010287         0.01507       0.0032331       0.0032937
v  Dissip              9.2141e-05        0.032577      0.00044819      0.00038716
v  TurbVisc                0.1678          11.355           4.627          5.1851
v  total_pressure           83076      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               64:        0.97535E-01

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


 INSTANT    0.650000000E+02   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998150E+04
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 :  0.23740E+00 0.12585E+01
   Friction velocity        uet   :  0.14202E-01 0.73539E-01
   Friction velocity        uk    :  0.17567E-01 0.38407E-01
   Dimensionless distance   yplus :  0.43161E+03 0.95308E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66411E+01      63   0.12794E-02   0.21753E-01 
c  VelocityX    0.46278E+04      12   0.66071E-02   0.38708E-03 
c  VelocityY    0.46278E+04      12   0.66071E-02   0.39323E-04 
c  VelocityZ    0.46278E+04      12   0.66071E-02   0.35999E-04 
c  TurbEner     0.58881E+01      16   0.75769E-04   0.79623E-08 
c  Dissip       0.15414E+01      14   0.49739E-03   0.42572E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.57           54521           26773           27267
v  Velocity[x]             0.2934          2.1622         0.90802         0.90981
v  Velocity[y]           -0.36675          0.7014      0.00059859      0.00038106
v  Velocity[z]           -0.42127         0.50806      -0.0013131      -0.0014305
v  TurbEner             0.0010262        0.014911         0.00324       0.0033005
v  Dissip              9.2116e-05        0.032247      0.00044894      0.00038783
v  TurbVisc               0.16708          11.329          4.6366          5.1954
v  total_pressure           83081      1.5656e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               65:        0.97481E-01

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


 INSTANT    0.660000000E+02   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000784E+04
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 :  0.23775E+00 0.13249E+01
   Friction velocity        uet   :  0.14222E-01 0.78986E-01
   Friction velocity        uk    :  0.17546E-01 0.38469E-01
   Dimensionless distance   yplus :  0.43156E+03 0.95444E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62334E+01      52   0.13162E-02   0.20431E-01 
c  VelocityX    0.46281E+04      12   0.77485E-02   0.34704E-03 
c  VelocityY    0.46281E+04      12   0.77485E-02   0.34051E-04 
c  VelocityZ    0.46281E+04      12   0.77485E-02   0.44323E-04 
c  TurbEner     0.58998E+01      16   0.81004E-04   0.67670E-08 
c  Dissip       0.15576E+01      15   0.67692E-03   0.11797E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.81           54519           26774           27268
v  Velocity[x]            0.29265          2.1827         0.90807         0.90985
v  Velocity[y]           -0.38289         0.69103      0.00058268       0.0003706
v  Velocity[z]           -0.42181         0.51214      -0.0013189      -0.0014358
v  TurbEner             0.0010187        0.015024        0.003246       0.0033065
v  Dissip              9.2098e-05        0.032498      0.00044972      0.00038851
v  TurbVisc               0.16707          11.323          4.6453          5.2045
v  total_pressure           83076      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               66:        0.95512E-01

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


 INSTANT    0.670000000E+02   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999281E+04
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 :  0.23759E+00 0.12818E+01
   Friction velocity        uet   :  0.14211E-01 0.74620E-01
   Friction velocity        uk    :  0.17482E-01 0.38445E-01
   Dimensionless distance   yplus :  0.43030E+03 0.95548E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69551E+01      57   0.15557E-02   0.22804E-01 
c  VelocityX    0.46282E+04      13   0.65584E-02   0.48467E-03 
c  VelocityY    0.46282E+04      13   0.65584E-02   0.26413E-04 
c  VelocityZ    0.46282E+04      13   0.65584E-02   0.12182E-03 
c  TurbEner     0.59102E+01      16   0.13411E-03   0.61265E-08 
c  Dissip       0.15738E+01      16   0.19593E-02   0.41628E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.95           54511           26774           27268
v  Velocity[x]            0.29248          2.0274         0.90803         0.90981
v  Velocity[y]           -0.36837          0.6991       0.0006095      0.00039174
v  Velocity[z]           -0.42287         0.50501       -0.001307      -0.0014247
v  TurbEner             0.0010186        0.015613       0.0032515       0.0033118
v  Dissip              9.2114e-05        0.034053       0.0004505      0.00038917
v  TurbVisc               0.16618          11.349          4.6531          5.2128
v  total_pressure           83082      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               67:        0.96359E-01

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


 INSTANT    0.680000000E+02   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000322E+04
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 :  0.23760E+00 0.13237E+01
   Friction velocity        uet   :  0.14211E-01 0.78908E-01
   Friction velocity        uk    :  0.17481E-01 0.38521E-01
   Dimensionless distance   yplus :  0.42947E+03 0.95618E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54493E+01      55   0.11404E-02   0.17863E-01 
c  VelocityX    0.46284E+04      12   0.64561E-02   0.33250E-03 
c  VelocityY    0.46284E+04      12   0.64561E-02   0.24641E-04 
c  VelocityZ    0.46284E+04      12   0.64561E-02   0.46990E-04 
c  TurbEner     0.59166E+01      16   0.15275E-03   0.60692E-08 
c  Dissip       0.15302E+01      16   0.24628E-02   0.79879E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.65           54509           26775           27269
v  Velocity[x]            0.29306          2.1037         0.90804         0.90983
v  Velocity[y]           -0.38271          0.6939      0.00058624      0.00037143
v  Velocity[z]           -0.42106         0.51233      -0.0013057      -0.0014222
v  TurbEner             0.0010168        0.014933       0.0032559       0.0033162
v  Dissip              9.2063e-05        0.032349      0.00045071      0.00038939
v  TurbVisc               0.16591           11.33          4.6601          5.2201
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               68:        0.96456E-01

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


 INSTANT    0.690000000E+02   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998233E+04
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 :  0.23796E+00 0.12236E+01
   Friction velocity        uet   :  0.14232E-01 0.72266E-01
   Friction velocity        uk    :  0.17466E-01 0.38638E-01
   Dimensionless distance   yplus :  0.42948E+03 0.95657E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58682E+01      54   0.14305E-02   0.19233E-01 
c  VelocityX    0.46286E+04      13   0.73510E-02   0.30905E-03 
c  VelocityY    0.46286E+04      13   0.73510E-02   0.21595E-04 
c  VelocityZ    0.46286E+04      13   0.73510E-02   0.31473E-04 
c  TurbEner     0.59247E+01      15   0.73643E-04   0.35318E-08 
c  Dissip       0.15326E+01      14   0.48828E-03   0.33928E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -178.7           54515           26775           27269
v  Velocity[x]             0.2929          2.1569         0.90803         0.90981
v  Velocity[y]           -0.36671         0.70314      0.00059441      0.00037551
v  Velocity[z]           -0.42322         0.50642      -0.0013107      -0.0014276
v  TurbEner             0.0010123        0.014814       0.0032598       0.0033201
v  Dissip              9.2062e-05        0.032028      0.00045102      0.00038969
v  TurbVisc               0.16592          11.335          4.6663          5.2266
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               69:        0.96389E-01

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


 INSTANT    0.700000000E+02   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998877E+04
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 :  0.23807E+00 0.13246E+01
   Friction velocity        uet   :  0.14238E-01 0.78960E-01
   Friction velocity        uk    :  0.17427E-01 0.38680E-01
   Dimensionless distance   yplus :  0.42886E+03 0.95738E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73165E+01      58   0.17588E-02   0.23996E-01 
c  VelocityX    0.46287E+04      13   0.71183E-02   0.45490E-03 
c  VelocityY    0.46287E+04      13   0.71183E-02   0.45147E-04 
c  VelocityZ    0.46287E+04      13   0.71183E-02   0.39888E-04 
c  TurbEner     0.59316E+01      15   0.10360E-03   0.34839E-08 
c  Dissip       0.15354E+01      15   0.14445E-02   0.25115E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.21           54496           26776           27270
v  Velocity[x]            0.29267          1.9976         0.90806         0.90984
v  Velocity[y]            -0.3825         0.69012      0.00058926      0.00037342
v  Velocity[z]           -0.42346          0.5113      -0.0013038       -0.001419
v  TurbEner             0.0010119        0.015241       0.0032633       0.0033236
v  Dissip              9.2019e-05        0.033093       0.0004514      0.00039002
v  TurbVisc               0.16533          11.371          4.6719          5.2325
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP               70:        0.96713E-01

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


 INSTANT    0.710000000E+02   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997774E+04
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 :  0.23789E+00 0.12665E+01
   Friction velocity        uet   :  0.14226E-01 0.73823E-01
   Friction velocity        uk    :  0.17423E-01 0.38638E-01
   Dimensionless distance   yplus :  0.42783E+03 0.95799E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69103E+01      59   0.15173E-02   0.22642E-01 
c  VelocityX    0.46288E+04      12   0.68499E-02   0.41422E-03 
c  VelocityY    0.46288E+04      12   0.68499E-02   0.55226E-04 
c  VelocityZ    0.46288E+04      12   0.68499E-02   0.11511E-03 
c  TurbEner     0.59359E+01      15   0.14384E-03   0.40514E-08 
c  Dissip       0.14938E+01      17   0.26538E-02   0.93161E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.17           54515           26775           27270
v  Velocity[x]            0.29306          2.0887         0.90803          0.9098
v  Velocity[y]           -0.36724         0.69928      0.00060256      0.00038225
v  Velocity[z]           -0.42357          0.5048      -0.0012955      -0.0014121
v  TurbEner             0.0010125        0.014623       0.0032661       0.0033264
v  Dissip              9.2004e-05        0.031354      0.00045129         0.00039
v  TurbVisc               0.16491          11.352          4.6768          5.2376
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               71:        0.96192E-01

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


 INSTANT    0.720000000E+02   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001277E+04
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 :  0.23797E+00 0.13231E+01
   Friction velocity        uet   :  0.14230E-01 0.78858E-01
   Friction velocity        uk    :  0.17428E-01 0.38718E-01
   Dimensionless distance   yplus :  0.42844E+03 0.95829E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59486E+01      58   0.14229E-02   0.19505E-01 
c  VelocityX    0.46289E+04      12   0.73143E-02   0.34310E-03 
c  VelocityY    0.46289E+04      12   0.73143E-02   0.31636E-04 
c  VelocityZ    0.46289E+04      12   0.73143E-02   0.55667E-04 
c  TurbEner     0.59411E+01      14   0.71094E-04   0.21907E-08 
c  Dissip       0.14859E+01      14   0.84447E-03   0.84247E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.54           54514           26776           27270
v  Velocity[x]            0.29268          2.1359         0.90805         0.90983
v  Velocity[y]            -0.3825          0.6931      0.00059071      0.00037333
v  Velocity[z]           -0.42495         0.51187      -0.0013045      -0.0014214
v  TurbEner             0.0010074        0.014517       0.0032685       0.0033288
v  Dissip               9.202e-05        0.030791      0.00045134      0.00039007
v  TurbVisc               0.16521          11.354          4.6812          5.2422
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP               72:        0.95493E-01

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


 INSTANT    0.730000000E+02   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999030E+04
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 :  0.23785E+00 0.12155E+01
   Friction velocity        uet   :  0.14223E-01 0.72460E-01
   Friction velocity        uk    :  0.17384E-01 0.38724E-01
   Dimensionless distance   yplus :  0.42766E+03 0.95831E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61469E+01      53   0.13768E-02   0.20144E-01 
c  VelocityX    0.46291E+04      12   0.70137E-02   0.34266E-03 
c  VelocityY    0.46291E+04      12   0.70137E-02   0.22651E-04 
c  VelocityZ    0.46291E+04      12   0.70137E-02   0.35903E-04 
c  TurbEner     0.59467E+01      14   0.68562E-04   0.19669E-08 
c  Dissip       0.14950E+01      14   0.53661E-03   0.70372E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.07           54505           26775           27270
v  Velocity[x]             0.2928           2.178         0.90806         0.90983
v  Velocity[y]           -0.36689         0.70109      0.00059858      0.00037769
v  Velocity[z]           -0.42414         0.50574      -0.0012941       -0.001409
v  TurbEner             0.0010089        0.014589       0.0032708       0.0033311
v  Dissip              9.2023e-05        0.030776      0.00045153      0.00039023
v  TurbVisc                0.1645          11.329          4.6851          5.2462
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               73:        0.95497E-01

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


 INSTANT    0.740000000E+02   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001361E+04
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 :  0.23771E+00 0.13231E+01
   Friction velocity        uet   :  0.14214E-01 0.78865E-01
   Friction velocity        uk    :  0.17397E-01 0.38781E-01
   Dimensionless distance   yplus :  0.42715E+03 0.95845E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58257E+01      54   0.12219E-02   0.19095E-01 
c  VelocityX    0.46291E+04      12   0.72428E-02   0.38358E-03 
c  VelocityY    0.46291E+04      12   0.72428E-02   0.32513E-04 
c  VelocityZ    0.46291E+04      12   0.72428E-02   0.43489E-04 
c  TurbEner     0.59509E+01      14   0.12599E-03   0.23711E-08 
c  Dissip       0.15018E+01      15   0.16334E-02   0.27279E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.93           54505           26776           27270
v  Velocity[x]            0.29307          2.0127         0.90804         0.90982
v  Velocity[y]           -0.38294          0.6935      0.00059276      0.00037523
v  Velocity[z]           -0.42504         0.51039      -0.0013101      -0.0014272
v  TurbEner             0.0010081        0.015153       0.0032729       0.0033331
v  Dissip              9.2038e-05        0.032037      0.00045171       0.0003904
v  TurbVisc               0.16435          11.324          4.6886          5.2498
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               74:        0.95476E-01

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


 INSTANT    0.750000000E+02   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000477E+04
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 :  0.23784E+00 0.12401E+01
   Friction velocity        uet   :  0.14222E-01 0.72515E-01
   Friction velocity        uk    :  0.17390E-01 0.38825E-01
   Dimensionless distance   yplus :  0.42733E+03 0.95923E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66088E+01      58   0.15004E-02   0.21662E-01 
c  VelocityX    0.46293E+04      13   0.70176E-02   0.40356E-03 
c  VelocityY    0.46293E+04      13   0.70176E-02   0.44572E-04 
c  VelocityZ    0.46293E+04      13   0.70176E-02   0.10094E-03 
c  TurbEner     0.59530E+01      14   0.12184E-03   0.21414E-08 
c  Dissip       0.14599E+01      17   0.24733E-02   0.85587E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.38           54514           26775           27269
v  Velocity[x]            0.29267          2.0876         0.90805         0.90982
v  Velocity[y]            -0.3676         0.70004      0.00059074      0.00036999
v  Velocity[z]            -0.4255         0.50423      -0.0012993      -0.0014165
v  TurbEner             0.0010052        0.014638       0.0032743       0.0033345
v  Dissip              9.2074e-05        0.030478       0.0004515      0.00039028
v  TurbVisc                0.1644          11.352          4.6917           5.253
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               75:        0.96796E-01

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


 INSTANT    0.760000000E+02   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001590E+04
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 :  0.23763E+00 0.13247E+01
   Friction velocity        uet   :  0.14210E-01 0.78952E-01
   Friction velocity        uk    :  0.17365E-01 0.38856E-01
   Dimensionless distance   yplus :  0.42707E+03 0.95922E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63856E+01      57   0.15378E-02   0.20934E-01 
c  VelocityX    0.46293E+04      13   0.68474E-02   0.44232E-03 
c  VelocityY    0.46293E+04      13   0.68474E-02   0.29641E-04 
c  VelocityZ    0.46293E+04      13   0.68474E-02   0.52917E-04 
c  TurbEner     0.59565E+01      13   0.66403E-04   0.14061E-08 
c  Dissip       0.14570E+01      14   0.60431E-03   0.50030E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.57           54503           26775           27270
v  Velocity[x]            0.29249          2.1426         0.90807         0.90985
v  Velocity[y]           -0.38232          0.6932      0.00058945      0.00037058
v  Velocity[z]            -0.4226         0.51188      -0.0012919      -0.0014083
v  TurbEner             0.0010059        0.014587       0.0032758        0.003336
v  Dissip              9.2105e-05        0.030097      0.00045149       0.0003903
v  TurbVisc               0.16402          11.334          4.6942          5.2556
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               76:        0.96471E-01

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


 INSTANT    0.770000000E+02   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999690E+04
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 :  0.23734E+00 0.12141E+01
   Friction velocity        uet   :  0.14194E-01 0.72283E-01
   Friction velocity        uk    :  0.17372E-01 0.38861E-01
   Dimensionless distance   yplus :  0.42640E+03 0.95918E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60790E+01      53   0.11810E-02   0.19928E-01 
c  VelocityX    0.46294E+04      12   0.66764E-02   0.35218E-03 
c  VelocityY    0.46294E+04      12   0.66764E-02   0.25322E-04 
c  VelocityZ    0.46294E+04      12   0.66764E-02   0.30836E-04 
c  TurbEner     0.59595E+01      13   0.90005E-04   0.17383E-08 
c  Dissip       0.14736E+01      15   0.68388E-03   0.10748E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.43           54505           26775           27269
v  Velocity[x]            0.29301          2.1834         0.90804         0.90981
v  Velocity[y]           -0.36612         0.70157      0.00058816      0.00036523
v  Velocity[z]           -0.42359         0.50651       -0.001292      -0.0014072
v  TurbEner             0.0010078        0.014732       0.0032771       0.0033372
v  Dissip              9.2088e-05        0.030337      0.00045163       0.0003904
v  TurbVisc               0.16375          11.324          4.6966           5.258
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               77:        0.95548E-01

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


 INSTANT    0.780000000E+02   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001977E+04
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 :  0.23774E+00 0.13245E+01
   Friction velocity        uet   :  0.14219E-01 0.78952E-01
   Friction velocity        uk    :  0.17388E-01 0.38829E-01
   Dimensionless distance   yplus :  0.42731E+03 0.95919E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65557E+01      54   0.16421E-02   0.21504E-01 
c  VelocityX    0.46294E+04      12   0.72803E-02   0.34934E-03 
c  VelocityY    0.46294E+04      12   0.72803E-02   0.38142E-04 
c  VelocityZ    0.46294E+04      12   0.72803E-02   0.37669E-04 
c  TurbEner     0.59624E+01      13   0.12171E-03   0.17030E-08 
c  Dissip       0.14851E+01      16   0.18743E-02   0.37380E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.78           54511           26775           27269
v  Velocity[x]            0.29287          2.0099         0.90805         0.90982
v  Velocity[y]           -0.38237         0.69133      0.00057771      0.00036083
v  Velocity[z]           -0.42386         0.51105      -0.0012993      -0.0014178
v  TurbEner             0.0010038        0.015323       0.0032783       0.0033383
v  Dissip              9.2098e-05         0.03179      0.00045182      0.00039055
v  TurbVisc               0.16421          11.362          4.6986            5.26
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               78:        0.95930E-01

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


 INSTANT    0.790000000E+02   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998821E+04
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 :  0.23802E+00 0.12512E+01
   Friction velocity        uet   :  0.14237E-01 0.72970E-01
   Friction velocity        uk    :  0.17353E-01 0.38770E-01
   Dimensionless distance   yplus :  0.42675E+03 0.95924E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71976E+01      59   0.15776E-02   0.23593E-01 
c  VelocityX    0.46294E+04      13   0.75111E-02   0.39539E-03 
c  VelocityY    0.46294E+04      13   0.75111E-02   0.61291E-04 
c  VelocityZ    0.46294E+04      13   0.75111E-02   0.12630E-03 
c  TurbEner     0.59632E+01      14   0.12298E-03   0.21508E-08 
c  Dissip       0.14557E+01      16   0.20860E-02   0.63563E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.69           54516           26775           27269
v  Velocity[x]            0.29259          2.0949         0.90804         0.90981
v  Velocity[y]           -0.36799          0.6987      0.00059783      0.00037612
v  Velocity[z]           -0.42426         0.50402      -0.0012743      -0.0013928
v  TurbEner             0.0010066        0.014804       0.0032789        0.003339
v  Dissip               9.209e-05        0.030465      0.00045161      0.00039042
v  TurbVisc                0.1637          11.344          4.7004          5.2618
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               79:        0.97015E-01

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


 INSTANT    0.800000000E+02   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001028E+04
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 :  0.23763E+00 0.13235E+01
   Friction velocity        uet   :  0.14215E-01 0.78890E-01
   Friction velocity        uk    :  0.17378E-01 0.38805E-01
   Dimensionless distance   yplus :  0.42649E+03 0.95903E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.74583E+01      67   0.14585E-02   0.24445E-01 
c  VelocityX    0.46295E+04      12   0.69993E-02   0.44464E-03 
c  VelocityY    0.46295E+04      12   0.69993E-02   0.47543E-04 
c  VelocityZ    0.46295E+04      12   0.69993E-02   0.62986E-04 
c  TurbEner     0.59645E+01      13   0.66278E-04   0.11357E-08 
c  Dissip       0.14568E+01      14   0.49594E-03   0.42812E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.03           54505           26775           27270
v  Velocity[x]            0.29303          2.1382         0.90805         0.90982
v  Velocity[y]           -0.38252         0.69206      0.00057767       0.0003578
v  Velocity[z]           -0.42572         0.51174      -0.0012869      -0.0014046
v  TurbEner             0.0010075        0.014756       0.0032796       0.0033397
v  Dissip              9.2078e-05        0.030201      0.00045156      0.00039038
v  TurbVisc               0.16369          11.342          4.7019          5.2633
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               80:        0.98004E-01

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


 INSTANT    0.810000000E+02   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999238E+04
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 :  0.23772E+00 0.12157E+01
   Friction velocity        uet   :  0.14222E-01 0.72475E-01
   Friction velocity        uk    :  0.17386E-01 0.38771E-01
   Dimensionless distance   yplus :  0.42707E+03 0.95943E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72246E+01      58   0.14399E-02   0.23672E-01 
c  VelocityX    0.46297E+04      12   0.74186E-02   0.34606E-03 
c  VelocityY    0.46297E+04      12   0.74186E-02   0.45078E-04 
c  VelocityZ    0.46297E+04      12   0.74186E-02   0.34590E-04 
c  TurbEner     0.59673E+01      13   0.69743E-04   0.10046E-08 
c  Dissip       0.14770E+01      15   0.79094E-03   0.14688E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.97           54511           26775           27269
v  Velocity[x]            0.29265          2.1838         0.90807         0.90984
v  Velocity[y]           -0.36606         0.70063      0.00057951      0.00035683
v  Velocity[z]           -0.42269         0.50635      -0.0012848       -0.001403
v  TurbEner             0.0010058        0.014851       0.0032803       0.0033403
v  Dissip              9.2082e-05        0.030434      0.00045172      0.00039049
v  TurbVisc               0.16402          11.375          4.7033          5.2647
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               81:        0.96626E-01

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


 INSTANT    0.820000000E+02   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001708E+04
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 :  0.23773E+00 0.13233E+01
   Friction velocity        uet   :  0.14223E-01 0.78882E-01
   Friction velocity        uk    :  0.17370E-01 0.38828E-01
   Dimensionless distance   yplus :  0.42703E+03 0.95957E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67040E+01      58   0.16078E-02   0.21985E-01 
c  VelocityX    0.46296E+04      12   0.72620E-02   0.43994E-03 
c  VelocityY    0.46296E+04      12   0.72620E-02   0.31127E-04 
c  VelocityZ    0.46296E+04      12   0.72620E-02   0.44007E-04 
c  TurbEner     0.59692E+01      14   0.12423E-03   0.17634E-08 
c  Dissip       0.14900E+01      16   0.19465E-02   0.41496E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.88           54490           26775           27269
v  Velocity[x]            0.29253          2.0121         0.90808         0.90985
v  Velocity[y]           -0.38247         0.69294      0.00057549      0.00036059
v  Velocity[z]           -0.42186         0.51074      -0.0013005      -0.0014159
v  TurbEner             0.0010078        0.015434       0.0032813       0.0033411
v  Dissip              9.2116e-05        0.031952      0.00045195      0.00039068
v  TurbVisc               0.16392          11.354          4.7044          5.2659
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               82:        0.95902E-01

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


 INSTANT    0.830000000E+02   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999125E+04
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 :  0.23735E+00 0.12442E+01
   Friction velocity        uet   :  0.14201E-01 0.72552E-01
   Friction velocity        uk    :  0.17388E-01 0.38863E-01
   Dimensionless distance   yplus :  0.42654E+03 0.95933E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64143E+01      64   0.13371E-02   0.21016E-01 
c  VelocityX    0.46296E+04      12   0.67267E-02   0.36790E-03 
c  VelocityY    0.46296E+04      12   0.67267E-02   0.29708E-04 
c  VelocityZ    0.46296E+04      12   0.67267E-02   0.10061E-03 
c  TurbEner     0.59689E+01      14   0.13059E-03   0.22612E-08 
c  Dissip       0.14624E+01      16   0.19851E-02   0.60541E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.76           54504           26774           27268
v  Velocity[x]            0.29337          2.0918         0.90805         0.90982
v  Velocity[y]           -0.36812             0.7      0.00058398      0.00036496
v  Velocity[z]           -0.42085         0.50387      -0.0012837      -0.0014012
v  TurbEner             0.0010103        0.014905       0.0032816       0.0033415
v  Dissip              9.2131e-05        0.030717      0.00045174      0.00039052
v  TurbVisc               0.16371           11.35          4.7056           5.267
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               83:        0.97273E-01

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


 INSTANT    0.840000000E+02   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002558E+04
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 :  0.23769E+00 0.13252E+01
   Friction velocity        uet   :  0.14223E-01 0.78987E-01
   Friction velocity        uk    :  0.17409E-01 0.38844E-01
   Dimensionless distance   yplus :  0.42754E+03 0.95979E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59730E+01      55   0.14470E-02   0.19589E-01 
c  VelocityX    0.46297E+04      13   0.71546E-02   0.35693E-03 
c  VelocityY    0.46297E+04      13   0.71546E-02   0.27747E-04 
c  VelocityZ    0.46297E+04      13   0.71546E-02   0.51302E-04 
c  TurbEner     0.59700E+01      13   0.72669E-04   0.94392E-09 
c  Dissip       0.14644E+01      14   0.52783E-03   0.41754E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.48           54508           26775           27269
v  Velocity[x]            0.29272          2.1406         0.90808         0.90985
v  Velocity[y]           -0.38288         0.69291      0.00057047      0.00035446
v  Velocity[z]            -0.4229         0.51131      -0.0012929      -0.0014113
v  TurbEner              0.001007        0.014791       0.0032822       0.0033419
v  Dissip               9.214e-05        0.030414      0.00045175      0.00039052
v  TurbVisc               0.16428          11.325          4.7064          5.2678
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               84:        0.96434E-01

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


 INSTANT    0.850000000E+02   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998331E+04
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 :  0.23823E+00 0.12151E+01
   Friction velocity        uet   :  0.14256E-01 0.72275E-01
   Friction velocity        uk    :  0.17381E-01 0.38757E-01
   Dimensionless distance   yplus :  0.42722E+03 0.95945E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66493E+01      62   0.14811E-02   0.21800E-01 
c  VelocityX    0.46298E+04      13   0.72897E-02   0.46323E-03 
c  VelocityY    0.46298E+04      13   0.72897E-02   0.25067E-04 
c  VelocityZ    0.46298E+04      13   0.72897E-02   0.38948E-04 
c  TurbEner     0.59716E+01      13   0.71583E-04   0.10875E-08 
c  Dissip       0.14837E+01      15   0.71047E-03   0.12139E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.45           54505           26775           27269
v  Velocity[x]             0.2924          2.1824         0.90806         0.90983
v  Velocity[y]           -0.36815         0.70136      0.00058265      0.00036462
v  Velocity[z]           -0.42188         0.50683      -0.0012784      -0.0013936
v  TurbEner             0.0010101        0.014863       0.0032826       0.0033423
v  Dissip              9.2145e-05        0.030621      0.00045185      0.00039059
v  TurbVisc               0.16402          11.338          4.7072          5.2686
v  total_pressure           83080      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               85:        0.97265E-01

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


 INSTANT    0.860000000E+02   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000174E+04
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 :  0.23747E+00 0.13246E+01
   Friction velocity        uet   :  0.14211E-01 0.78961E-01
   Friction velocity        uk    :  0.17408E-01 0.38775E-01
   Dimensionless distance   yplus :  0.42716E+03 0.95868E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65760E+01      58   0.13855E-02   0.21563E-01 
c  VelocityX    0.46296E+04      12   0.68937E-02   0.43280E-03 
c  VelocityY    0.46296E+04      12   0.68937E-02   0.41538E-04 
c  VelocityZ    0.46296E+04      12   0.68937E-02   0.36509E-04 
c  TurbEner     0.59720E+01      13   0.11838E-03   0.16570E-08 
c  Dissip       0.14947E+01      16   0.18843E-02   0.38377E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.21           54503           26775           27269
v  Velocity[x]            0.29275          2.0082         0.90806         0.90984
v  Velocity[y]           -0.38296          0.6921      0.00057217      0.00035535
v  Velocity[z]           -0.42242         0.51374      -0.0012843      -0.0014003
v  TurbEner             0.0010092        0.015422       0.0032829       0.0033426
v  Dissip              9.2138e-05        0.032094      0.00045198      0.00039068
v  TurbVisc               0.16405          11.305          4.7079          5.2692
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               86:        0.96467E-01

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


 INSTANT    0.870000000E+02   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999474E+04
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 :  0.23819E+00 0.12335E+01
   Friction velocity        uet   :  0.14255E-01 0.72406E-01
   Friction velocity        uk    :  0.17400E-01 0.38802E-01
   Dimensionless distance   yplus :  0.42739E+03 0.95849E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62757E+01      57   0.14901E-02   0.20570E-01 
c  VelocityX    0.46298E+04      12   0.70700E-02   0.32721E-03 
c  VelocityY    0.46298E+04      12   0.70700E-02   0.44417E-04 
c  VelocityZ    0.46298E+04      12   0.70700E-02   0.61766E-04 
c  TurbEner     0.59718E+01      14   0.13190E-03   0.19262E-08 
c  Dissip       0.14640E+01      16   0.20920E-02   0.65006E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.84           54511           26774           27268
v  Velocity[x]             0.2929          2.0908         0.90805         0.90982
v  Velocity[y]           -0.36667         0.69904      0.00057983      0.00036044
v  Velocity[z]           -0.42311         0.50783      -0.0012819      -0.0013985
v  TurbEner             0.0010085        0.014863       0.0032829       0.0033427
v  Dissip              9.2137e-05        0.030772      0.00045169      0.00039048
v  TurbVisc               0.16422          11.304          4.7084          5.2697
v  total_pressure           83080      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP               87:        0.96866E-01

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


 INSTANT    0.880000000E+02   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002020E+04
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 :  0.23811E+00 0.13232E+01
   Friction velocity        uet   :  0.14251E-01 0.78880E-01
   Friction velocity        uk    :  0.17394E-01 0.38714E-01
   Dimensionless distance   yplus :  0.42750E+03 0.95768E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62949E+01      57   0.15275E-02   0.20647E-01 
c  VelocityX    0.46298E+04      12   0.65824E-02   0.31834E-03 
c  VelocityY    0.46298E+04      12   0.65824E-02   0.32233E-04 
c  VelocityZ    0.46298E+04      12   0.65824E-02   0.41031E-04 
c  TurbEner     0.59722E+01      13   0.68437E-04   0.96110E-09 
c  Dissip       0.14659E+01      14   0.51464E-03   0.40534E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.06           54492           26775           27269
v  Velocity[x]            0.29263          2.1383         0.90807         0.90984
v  Velocity[y]           -0.38271         0.69105      0.00057655      0.00036111
v  Velocity[z]            -0.4248         0.51214      -0.0012722      -0.0013883
v  TurbEner             0.0010114        0.014757       0.0032831        0.003343
v  Dissip              9.2094e-05        0.030479      0.00045162      0.00039043
v  TurbVisc               0.16429          11.332          4.7089          5.2702
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               88:        0.96613E-01

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


 INSTANT    0.890000000E+02   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998172E+04
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 :  0.23751E+00 0.12632E+01
   Friction velocity        uet   :  0.14215E-01 0.73657E-01
   Friction velocity        uk    :  0.17419E-01 0.38768E-01
   Dimensionless distance   yplus :  0.42722E+03 0.95673E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61980E+01      55   0.11744E-02   0.20308E-01 
c  VelocityX    0.46298E+04      12   0.75726E-02   0.33333E-03 
c  VelocityY    0.46298E+04      12   0.75726E-02   0.30661E-04 
c  VelocityZ    0.46298E+04      12   0.75726E-02   0.38695E-04 
c  TurbEner     0.59732E+01      12   0.67581E-04   0.92170E-09 
c  Dissip       0.14900E+01      15   0.72426E-03   0.12753E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.68           54513           26775           27269
v  Velocity[x]            0.29303          2.1851         0.90806         0.90984
v  Velocity[y]           -0.36801         0.69932      0.00057733      0.00035567
v  Velocity[z]           -0.42431         0.50497      -0.0012729      -0.0013893
v  TurbEner             0.0010153        0.014838       0.0032833       0.0033431
v  Dissip              9.2052e-05        0.030681      0.00045173      0.00039049
v  TurbVisc               0.16427          11.319          4.7093          5.2706
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               89:        0.96429E-01

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


 INSTANT    0.900000000E+02   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000507E+04
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 :  0.23792E+00 0.13225E+01
   Friction velocity        uet   :  0.14240E-01 0.78844E-01
   Friction velocity        uk    :  0.17452E-01 0.38771E-01
   Dimensionless distance   yplus :  0.42852E+03 0.95692E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61652E+01      53   0.17136E-02   0.20226E-01 
c  VelocityX    0.46298E+04      12   0.68977E-02   0.37795E-03 
c  VelocityY    0.46298E+04      12   0.68977E-02   0.27630E-04 
c  VelocityZ    0.46298E+04      12   0.68977E-02   0.94945E-04 
c  TurbEner     0.59740E+01      13   0.11553E-03   0.13091E-08 
c  Dissip       0.15010E+01      16   0.17992E-02   0.36724E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.33           54514           26775           27270
v  Velocity[x]            0.29259          2.0229         0.90805         0.90983
v  Velocity[y]           -0.38271         0.69204      0.00057836      0.00036089
v  Velocity[z]           -0.42463         0.51222      -0.0012788      -0.0013975
v  TurbEner             0.0010128          0.0154       0.0032835       0.0033433
v  Dissip              9.2052e-05        0.032074      0.00045186      0.00039059
v  TurbVisc               0.16506          11.325          4.7096          5.2709
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               90:        0.96210E-01

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


 INSTANT    0.910000000E+02   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998365E+04
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 :  0.23764E+00 0.12469E+01
   Friction velocity        uet   :  0.14224E-01 0.72700E-01
   Friction velocity        uk    :  0.17431E-01 0.38680E-01
   Dimensionless distance   yplus :  0.42833E+03 0.95714E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61693E+01      55   0.14953E-02   0.20231E-01 
c  VelocityX    0.46298E+04      12   0.65102E-02   0.32986E-03 
c  VelocityY    0.46298E+04      12   0.65102E-02   0.27264E-04 
c  VelocityZ    0.46298E+04      12   0.65102E-02   0.56815E-04 
c  TurbEner     0.59729E+01      14   0.12526E-03   0.19982E-08 
c  Dissip       0.14687E+01      16   0.19954E-02   0.63494E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.39           54511           26775           27270
v  Velocity[x]            0.29275          2.0965         0.90805         0.90982
v  Velocity[y]           -0.36671         0.69946      0.00058951      0.00036847
v  Velocity[z]           -0.42495         0.50643      -0.0012646      -0.0013781
v  TurbEner             0.0010166        0.014884       0.0032833       0.0033432
v  Dissip              9.2059e-05        0.030866      0.00045157      0.00039039
v  TurbVisc               0.16491          11.365          4.7099          5.2712
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               91:        0.95851E-01

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


 INSTANT    0.920000000E+02   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000421E+04
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 :  0.23738E+00 0.13243E+01
   Friction velocity        uet   :  0.14208E-01 0.78949E-01
   Friction velocity        uk    :  0.17463E-01 0.38695E-01
   Dimensionless distance   yplus :  0.42838E+03 0.95680E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60291E+01      55   0.11677E-02   0.19761E-01 
c  VelocityX    0.46298E+04      12   0.66552E-02   0.36341E-03 
c  VelocityY    0.46298E+04      12   0.66552E-02   0.24648E-04 
c  VelocityZ    0.46298E+04      12   0.66552E-02   0.44595E-04 
c  TurbEner     0.59728E+01      13   0.65673E-04   0.89431E-09 
c  Dissip       0.14734E+01      14   0.42988E-03   0.35526E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.95           54500           26776           27270
v  Velocity[x]            0.29298           2.147         0.90805         0.90983
v  Velocity[y]           -0.38236         0.69147      0.00057753       0.0003579
v  Velocity[z]           -0.42365         0.51127       -0.001273      -0.0013918
v  TurbEner             0.0010178        0.014783       0.0032834       0.0033433
v  Dissip              9.2063e-05         0.03067      0.00045152      0.00039034
v  TurbVisc               0.16502          11.346          4.7101          5.2714
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP               92:        0.95506E-01

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


 INSTANT    0.930000000E+02   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998760E+04
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 :  0.23773E+00 0.12333E+01
   Friction velocity        uet   :  0.14229E-01 0.72408E-01
   Friction velocity        uk    :  0.17474E-01 0.38750E-01
   Dimensionless distance   yplus :  0.42910E+03 0.95696E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64602E+01      60   0.13544E-02   0.21174E-01 
c  VelocityX    0.46299E+04      12   0.66991E-02   0.36526E-03 
c  VelocityY    0.46299E+04      12   0.66991E-02   0.36542E-04 
c  VelocityZ    0.46299E+04      12   0.66991E-02   0.35936E-04 
c  TurbEner     0.59740E+01      12   0.66717E-04   0.72237E-09 
c  Dissip       0.14991E+01      15   0.80770E-03   0.15041E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.98           54518           26775           27269
v  Velocity[x]            0.29256          2.1874         0.90805         0.90982
v  Velocity[y]           -0.36706         0.70023      0.00058269      0.00036083
v  Velocity[z]             -0.424         0.50486      -0.0012783      -0.0013938
v  TurbEner             0.0010151        0.014872       0.0032833       0.0033433
v  Dissip              9.2085e-05        0.030955      0.00045161      0.00039039
v  TurbVisc               0.16545          11.352          4.7104          5.2718
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               93:        0.96114E-01

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


 INSTANT    0.940000000E+02   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001279E+04
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 :  0.23747E+00 0.13226E+01
   Friction velocity        uet   :  0.14213E-01 0.78837E-01
   Friction velocity        uk    :  0.17451E-01 0.38800E-01
   Dimensionless distance   yplus :  0.42894E+03 0.95690E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61110E+01      54   0.14258E-02   0.20035E-01 
c  VelocityX    0.46297E+04      12   0.63104E-02   0.37907E-03 
c  VelocityY    0.46297E+04      12   0.63104E-02   0.40255E-04 
c  VelocityZ    0.46297E+04      12   0.63104E-02   0.35642E-04 
c  TurbEner     0.59744E+01      13   0.11554E-03   0.13802E-08 
c  Dissip       0.15114E+01      16   0.19764E-02   0.45303E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.54           54533           26775           27270
v  Velocity[x]            0.29272          2.0157         0.90805         0.90982
v  Velocity[y]            -0.3825         0.69219      0.00057411      0.00035343
v  Velocity[z]           -0.42542         0.51184       -0.001286      -0.0014028
v  TurbEner             0.0010166        0.015444       0.0032836       0.0033434
v  Dissip              9.2117e-05        0.032477       0.0004518      0.00039052
v  TurbVisc                0.1653          11.331          4.7106          5.2719
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               94:        0.95126E-01

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


 INSTANT    0.950000000E+02   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998489E+04
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 :  0.23744E+00 0.12258E+01
   Friction velocity        uet   :  0.14212E-01 0.72466E-01
   Friction velocity        uk    :  0.17464E-01 0.38786E-01
   Dimensionless distance   yplus :  0.42838E+03 0.95753E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61887E+01      52   0.13505E-02   0.20283E-01 
c  VelocityX    0.46298E+04      12   0.73769E-02   0.32348E-03 
c  VelocityY    0.46298E+04      12   0.73769E-02   0.31980E-04 
c  VelocityZ    0.46298E+04      12   0.73769E-02   0.58255E-04 
c  TurbEner     0.59735E+01      14   0.12969E-03   0.18528E-08 
c  Dissip       0.14809E+01      16   0.20888E-02   0.67055E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.42           54543           26775           27269
v  Velocity[x]            0.29281          2.0945         0.90805         0.90983
v  Velocity[y]           -0.36694         0.69909      0.00057624       0.0003539
v  Velocity[z]           -0.42332         0.50575      -0.0012798      -0.0013953
v  TurbEner             0.0010188         0.01491       0.0032834       0.0033433
v  Dissip              9.2149e-05        0.031185      0.00045158      0.00039037
v  TurbVisc               0.16507          11.328          4.7108          5.2722
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               95:        0.94900E-01

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


 INSTANT    0.960000000E+02   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000692E+04
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 :  0.23755E+00 0.13247E+01
   Friction velocity        uet   :  0.14219E-01 0.78960E-01
   Friction velocity        uk    :  0.17482E-01 0.38775E-01
   Dimensionless distance   yplus :  0.42934E+03 0.95739E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57026E+01      53   0.12141E-02   0.18701E-01 
c  VelocityX    0.46299E+04      13   0.66430E-02   0.34356E-03 
c  VelocityY    0.46299E+04      13   0.66430E-02   0.32118E-04 
c  VelocityZ    0.46299E+04      13   0.66430E-02   0.86216E-04 
c  TurbEner     0.59740E+01      13   0.67260E-04   0.70237E-09 
c  Dissip       0.14854E+01      14   0.54309E-03   0.41306E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.82           54550           26775           27270
v  Velocity[x]            0.29277          2.1451         0.90806         0.90983
v  Velocity[y]           -0.38283         0.69305      0.00057495      0.00035453
v  Velocity[z]           -0.42163         0.51059      -0.0012739      -0.0013906
v  TurbEner             0.0010154        0.014818       0.0032836       0.0033435
v  Dissip              9.2174e-05         0.03086      0.00045158      0.00039037
v  TurbVisc               0.16565          11.358          4.7109          5.2723
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               96:        0.95285E-01

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


 INSTANT    0.970000000E+02   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999121E+04
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 :  0.23761E+00 0.12473E+01
   Friction velocity        uet   :  0.14222E-01 0.72757E-01
   Friction velocity        uk    :  0.17453E-01 0.38713E-01
   Dimensionless distance   yplus :  0.42896E+03 0.95719E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60651E+01      55   0.14943E-02   0.19880E-01 
c  VelocityX    0.46299E+04      13   0.72292E-02   0.37655E-03 
c  VelocityY    0.46299E+04      13   0.72292E-02   0.25727E-04 
c  VelocityZ    0.46299E+04      13   0.72292E-02   0.42178E-04 
c  TurbEner     0.59751E+01      13   0.74781E-04   0.96872E-09 
c  Dissip       0.15073E+01      15   0.84871E-03   0.15013E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.68           54542           26775           27269
v  Velocity[x]            0.29285          2.1819         0.90807         0.90984
v  Velocity[y]           -0.36736         0.70098      0.00058063      0.00035771
v  Velocity[z]           -0.42027         0.50438       -0.001268      -0.0013825
v  TurbEner             0.0010183        0.014979       0.0032837       0.0033435
v  Dissip              9.2179e-05        0.031286      0.00045177       0.0003905
v  TurbVisc               0.16539           11.34          4.7111          5.2725
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP               97:        0.95418E-01

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


 INSTANT    0.980000000E+02   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000141E+04
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 :  0.23753E+00 0.13240E+01
   Friction velocity        uet   :  0.14217E-01 0.78921E-01
   Friction velocity        uk    :  0.17478E-01 0.38765E-01
   Dimensionless distance   yplus :  0.42886E+03 0.95751E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64869E+01      60   0.15358E-02   0.21267E-01 
c  VelocityX    0.46299E+04      12   0.66566E-02   0.37583E-03 
c  VelocityY    0.46299E+04      12   0.66566E-02   0.24617E-04 
c  VelocityZ    0.46299E+04      12   0.66566E-02   0.44369E-04 
c  TurbEner     0.59764E+01      13   0.82035E-04   0.14277E-08 
c  Dissip       0.15366E+01      15   0.10389E-02   0.21065E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.29           54518           26776           27271
v  Velocity[x]            0.29275          2.2032         0.90806         0.90984
v  Velocity[y]            -0.3823         0.69087      0.00058234      0.00036348
v  Velocity[z]           -0.42196         0.51183      -0.0012654      -0.0013815
v  TurbEner             0.0010192        0.015166        0.003284       0.0033438
v  Dissip              9.2156e-05        0.031902      0.00045204      0.00039069
v  TurbVisc                0.1654          11.331          4.7112          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP               98:        0.95800E-01

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


 INSTANT    0.990000000E+02   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997961E+04
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 :  0.23792E+00 0.12165E+01
   Friction velocity        uet   :  0.14241E-01 0.72509E-01
   Friction velocity        uk    :  0.17486E-01 0.38816E-01
   Dimensionless distance   yplus :  0.42947E+03 0.95708E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64150E+01      54   0.13444E-02   0.21040E-01 
c  VelocityX    0.46299E+04      12   0.65525E-02   0.35627E-03 
c  VelocityY    0.46299E+04      12   0.65525E-02   0.39399E-04 
c  VelocityZ    0.46299E+04      12   0.65525E-02   0.56480E-04 
c  TurbEner     0.59766E+01      13   0.13241E-03   0.17191E-08 
c  Dissip       0.15603E+01      16   0.23507E-02   0.61775E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.55           54525           26776           27270
v  Velocity[x]            0.29256          2.0359         0.90804         0.90981
v  Velocity[y]           -0.36608         0.69908      0.00058513      0.00036336
v  Velocity[z]            -0.4229          0.5066      -0.0012766      -0.0013918
v  TurbEner             0.0010168         0.01582       0.0032843        0.003344
v  Dissip              9.2138e-05        0.033795      0.00045236      0.00039093
v  TurbVisc               0.16575          11.368          4.7114          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP               99:        0.95662E-01

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


 INSTANT    0.100000000E+03   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999741E+04
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 :  0.23789E+00 0.13233E+01
   Friction velocity        uet   :  0.14239E-01 0.78879E-01
   Friction velocity        uk    :  0.17465E-01 0.38834E-01
   Dimensionless distance   yplus :  0.42936E+03 0.95683E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65518E+01      53   0.12947E-02   0.21483E-01 
c  VelocityX    0.46298E+04      12   0.66088E-02   0.37357E-03 
c  VelocityY    0.46298E+04      12   0.66088E-02   0.48933E-04 
c  VelocityZ    0.46298E+04      12   0.66088E-02   0.47998E-04 
c  TurbEner     0.59751E+01      13   0.14417E-03   0.20555E-08 
c  Dissip       0.15284E+01      16   0.21064E-02   0.62100E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.99           54523           26777           27271
v  Velocity[x]            0.29278          2.1008         0.90805         0.90983
v  Velocity[y]           -0.38232         0.69237      0.00057468      0.00035644
v  Velocity[z]           -0.42281         0.51109      -0.0012815      -0.0013989
v  TurbEner             0.0010181        0.015176       0.0032843       0.0033439
v  Dissip              9.2101e-05        0.032349      0.00045221      0.00039082
v  TurbVisc               0.16559          11.351          4.7115          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              100:        0.96268E-01

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


 INSTANT    0.101000000E+03   TIME STEP NUMBER             101
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998485E+04
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 :  0.23792E+00 0.12714E+01
   Friction velocity        uet   :  0.14241E-01 0.74236E-01
   Friction velocity        uk    :  0.17476E-01 0.38830E-01
   Dimensionless distance   yplus :  0.42877E+03 0.95684E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65007E+01      56   0.14325E-02   0.21307E-01 
c  VelocityX    0.46299E+04      12   0.74960E-02   0.34142E-03 
c  VelocityY    0.46299E+04      12   0.74960E-02   0.33977E-04 
c  VelocityZ    0.46299E+04      12   0.74960E-02   0.33260E-04 
c  TurbEner     0.59755E+01      12   0.64790E-04   0.80323E-09 
c  Dissip       0.15354E+01      13   0.44091E-03   0.28784E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.58           54511           26776           27270
v  Velocity[x]            0.29303          2.1612         0.90807         0.90984
v  Velocity[y]           -0.36777         0.70145      0.00058749      0.00036599
v  Velocity[z]           -0.42375         0.50414      -0.0012648      -0.0013794
v  TurbEner             0.0010199        0.015026       0.0032843       0.0033439
v  Dissip              9.2118e-05        0.032067      0.00045224      0.00039084
v  TurbVisc                0.1653          11.353          4.7115          5.2728
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              101:        0.95737E-01

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


 INSTANT    0.102000000E+03   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001914E+04
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 :  0.23761E+00 0.13236E+01
   Friction velocity        uet   :  0.14222E-01 0.78893E-01
   Friction velocity        uk    :  0.17492E-01 0.38814E-01
   Dimensionless distance   yplus :  0.42972E+03 0.95695E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63643E+01      54   0.12645E-02   0.20873E-01 
c  VelocityX    0.46299E+04      12   0.71201E-02   0.38161E-03 
c  VelocityY    0.46299E+04      12   0.71201E-02   0.33723E-04 
c  VelocityZ    0.46299E+04      12   0.71201E-02   0.37372E-04 
c  TurbEner     0.59757E+01      14   0.85510E-04   0.16392E-08 
c  Dissip       0.15552E+01      15   0.79203E-03   0.15179E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.07           54511           26777           27271
v  Velocity[x]            0.29252          2.1849         0.90807         0.90984
v  Velocity[y]           -0.38248         0.69429      0.00056991       0.0003511
v  Velocity[z]           -0.42415         0.51172      -0.0012756      -0.0013927
v  TurbEner             0.0010156        0.015154       0.0032844        0.003344
v  Dissip              9.2115e-05         0.03241      0.00045243      0.00039096
v  TurbVisc               0.16581          11.328          4.7115          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              102:        0.95658E-01

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


 INSTANT    0.103000000E+03   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999796E+04
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 :  0.23769E+00 0.12165E+01
   Friction velocity        uet   :  0.14227E-01 0.72514E-01
   Friction velocity        uk    :  0.17455E-01 0.38756E-01
   Dimensionless distance   yplus :  0.42916E+03 0.95690E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62340E+01      60   0.14894E-02   0.20423E-01 
c  VelocityX    0.46299E+04      12   0.73557E-02   0.41416E-03 
c  VelocityY    0.46299E+04      12   0.73557E-02   0.24475E-04 
c  VelocityZ    0.46299E+04      12   0.73557E-02   0.41758E-04 
c  TurbEner     0.59762E+01      13   0.12027E-03   0.11561E-08 
c  Dissip       0.15711E+01      16   0.20831E-02   0.48167E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.21           54517           26776           27270
v  Velocity[x]            0.29277          2.0251         0.90806         0.90983
v  Velocity[y]           -0.36653         0.70013        0.000578      0.00035745
v  Velocity[z]           -0.42411         0.50597      -0.0012805      -0.0013978
v  TurbEner             0.0010177        0.015737       0.0032845        0.003344
v  Dissip              9.2127e-05        0.034064      0.00045267      0.00039113
v  TurbVisc               0.16539          11.322          4.7115          5.2728
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              103:        0.96527E-01

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


 INSTANT    0.104000000E+03   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001349E+04
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 :  0.23769E+00 0.13255E+01
   Friction velocity        uet   :  0.14226E-01 0.79008E-01
   Friction velocity        uk    :  0.17473E-01 0.38714E-01
   Dimensionless distance   yplus :  0.42880E+03 0.95710E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70701E+01      56   0.16451E-02   0.23186E-01 
c  VelocityX    0.46298E+04      12   0.70329E-02   0.39461E-03 
c  VelocityY    0.46298E+04      12   0.70329E-02   0.27398E-04 
c  VelocityZ    0.46298E+04      12   0.70329E-02   0.93929E-04 
c  TurbEner     0.59752E+01      14   0.15643E-03   0.21781E-08 
c  Dissip       0.15354E+01      16   0.24824E-02   0.79713E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.75           54518           26776           27270
v  Velocity[x]            0.29274          2.1043         0.90805         0.90984
v  Velocity[y]           -0.38227         0.69342      0.00057712      0.00035842
v  Velocity[z]           -0.42344         0.51103      -0.0012614      -0.0013802
v  TurbEner             0.0010179        0.015036       0.0032846       0.0033441
v  Dissip              9.2141e-05        0.032319      0.00045251      0.00039103
v  TurbVisc               0.16523          11.347          4.7115          5.2728
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              104:        0.95836E-01

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


 INSTANT    0.105000000E+03   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000067E+04
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 :  0.23738E+00 0.12506E+01
   Friction velocity        uet   :  0.14206E-01 0.73004E-01
   Friction velocity        uk    :  0.17475E-01 0.38770E-01
   Dimensionless distance   yplus :  0.42925E+03 0.95696E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62196E+01      54   0.13633E-02   0.20387E-01 
c  VelocityX    0.46298E+04      13   0.69342E-02   0.34244E-03 
c  VelocityY    0.46298E+04      13   0.69342E-02   0.43625E-04 
c  VelocityZ    0.46298E+04      13   0.69342E-02   0.57922E-04 
c  TurbEner     0.59746E+01      13   0.70536E-04   0.10034E-08 
c  Dissip       0.15328E+01      14   0.38555E-03   0.26573E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.29           54515           26775           27270
v  Velocity[x]            0.29284          2.1498         0.90805         0.90983
v  Velocity[y]            -0.3669           0.702      0.00058094      0.00035848
v  Velocity[z]           -0.42251         0.50476      -0.0012648      -0.0013823
v  TurbEner             0.0010148        0.014968       0.0032844        0.003344
v  Dissip              9.2124e-05        0.032087      0.00045247      0.00039099
v  TurbVisc               0.16547          11.329          4.7115          5.2728
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              105:        0.96334E-01

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


 INSTANT    0.106000000E+03   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001603E+04
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 :  0.23780E+00 0.13246E+01
   Friction velocity        uet   :  0.14230E-01 0.78959E-01
   Friction velocity        uk    :  0.17448E-01 0.38798E-01
   Dimensionless distance   yplus :  0.42902E+03 0.95663E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56194E+01      54   0.13944E-02   0.18428E-01 
c  VelocityX    0.46299E+04      12   0.72266E-02   0.36157E-03 
c  VelocityY    0.46299E+04      12   0.72266E-02   0.37126E-04 
c  VelocityZ    0.46299E+04      12   0.72266E-02   0.42943E-04 
c  TurbEner     0.59753E+01      12   0.74923E-04   0.71572E-09 
c  Dissip       0.15537E+01      15   0.73365E-03   0.13405E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.51           54517           26776           27270
v  Velocity[x]            0.29288          2.1921         0.90806         0.90984
v  Velocity[y]           -0.38235         0.69287      0.00058429      0.00036253
v  Velocity[z]           -0.42335         0.51177      -0.0012703      -0.0013896
v  TurbEner             0.0010154        0.015018       0.0032843       0.0033439
v  Dissip              9.2097e-05         0.03225      0.00045256      0.00039104
v  TurbVisc               0.16523          11.337          4.7115          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              106:        0.95737E-01

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


 INSTANT    0.107000000E+03   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998636E+04
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 :  0.23748E+00 0.12150E+01
   Friction velocity        uet   :  0.14210E-01 0.72424E-01
   Friction velocity        uk    :  0.17453E-01 0.38805E-01
   Dimensionless distance   yplus :  0.42828E+03 0.95689E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60009E+01      53   0.15321E-02   0.19668E-01 
c  VelocityX    0.46298E+04      12   0.66516E-02   0.40924E-03 
c  VelocityY    0.46298E+04      12   0.66516E-02   0.25568E-04 
c  VelocityZ    0.46298E+04      12   0.66516E-02   0.49606E-04 
c  TurbEner     0.59753E+01      13   0.12604E-03   0.13864E-08 
c  Dissip       0.15680E+01      16   0.21417E-02   0.49949E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.94           54507           26775           27270
v  Velocity[x]            0.29308          2.0251         0.90804         0.90982
v  Velocity[y]           -0.36682         0.69986      0.00059486       0.0003731
v  Velocity[z]           -0.42165         0.50575      -0.0012643      -0.0013793
v  TurbEner             0.0010162        0.015614       0.0032843       0.0033438
v  Dissip              9.2063e-05         0.03395      0.00045272      0.00039115
v  TurbVisc               0.16487          11.376          4.7114          5.2727
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              107:        0.95729E-01

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


 INSTANT    0.108000000E+03   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000756E+04
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 :  0.23700E+00 0.13240E+01
   Friction velocity        uet   :  0.14180E-01 0.78924E-01
   Friction velocity        uk    :  0.17461E-01 0.38784E-01
   Dimensionless distance   yplus :  0.42898E+03 0.95713E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56983E+01      54   0.11950E-02   0.18686E-01 
c  VelocityX    0.46297E+04      12   0.64317E-02   0.32962E-03 
c  VelocityY    0.46297E+04      12   0.64317E-02   0.27354E-04 
c  VelocityZ    0.46297E+04      12   0.64317E-02   0.37846E-04 
c  TurbEner     0.59733E+01      14   0.15788E-03   0.23664E-08 
c  Dissip       0.15281E+01      16   0.24608E-02   0.82946E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.16           54506           26776           27270
v  Velocity[x]            0.29248          2.0968         0.90804         0.90982
v  Velocity[y]           -0.38283         0.69132      0.00057499      0.00035575
v  Velocity[z]           -0.42188          0.5105      -0.0012803       -0.001397
v  TurbEner             0.0010116        0.014899        0.003284       0.0033436
v  Dissip               9.213e-05        0.032299      0.00045235      0.00039089
v  TurbVisc               0.16525           11.34          4.7113          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              108:        0.96332E-01

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


 INSTANT    0.109000000E+03   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998709E+04
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 :  0.23778E+00 0.12256E+01
   Friction velocity        uet   :  0.14226E-01 0.72440E-01
   Friction velocity        uk    :  0.17421E-01 0.38697E-01
   Dimensionless distance   yplus :  0.42833E+03 0.95661E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62588E+01      53   0.14111E-02   0.20516E-01 
c  VelocityX    0.46298E+04      12   0.74148E-02   0.33753E-03 
c  VelocityY    0.46298E+04      12   0.74148E-02   0.32608E-04 
c  VelocityZ    0.46298E+04      12   0.74148E-02   0.29673E-04 
c  TurbEner     0.59736E+01      12   0.64419E-04   0.62890E-09 
c  Dissip       0.15361E+01      13   0.42273E-03   0.27436E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.48           54516           26776           27270
v  Velocity[x]            0.29261          2.1563         0.90804         0.90982
v  Velocity[y]           -0.36736         0.70027      0.00058608      0.00036074
v  Velocity[z]           -0.42339         0.50437      -0.0012712       -0.001391
v  TurbEner             0.0010132        0.014755       0.0032838       0.0033434
v  Dissip              9.2127e-05        0.032047      0.00045225      0.00039082
v  TurbVisc               0.16477          11.332          4.7113          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              109:        0.94999E-01

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


 INSTANT    0.110000000E+03   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999914E+04
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 :  0.23776E+00 0.13231E+01
   Friction velocity        uet   :  0.14224E-01 0.78876E-01
   Friction velocity        uk    :  0.17435E-01 0.38679E-01
   Dimensionless distance   yplus :  0.42797E+03 0.95680E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62573E+01      53   0.14241E-02   0.20515E-01 
c  VelocityX    0.46297E+04      12   0.76149E-02   0.37156E-03 
c  VelocityY    0.46297E+04      12   0.76149E-02   0.30389E-04 
c  VelocityZ    0.46297E+04      12   0.76149E-02   0.81169E-04 
c  TurbEner     0.59741E+01      13   0.72818E-04   0.10194E-08 
c  Dissip       0.15557E+01      15   0.74476E-03   0.13573E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.39           54519           26776           27270
v  Velocity[x]            0.29323          2.1865         0.90804         0.90983
v  Velocity[y]           -0.38226         0.69325      0.00058348      0.00036292
v  Velocity[z]           -0.42084         0.51191      -0.0012555      -0.0013732
v  TurbEner             0.0010129        0.014845       0.0032837       0.0033434
v  Dissip              9.2114e-05        0.032262      0.00045236      0.00039089
v  TurbVisc               0.16464          11.358          4.7112          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              110:        0.95561E-01

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


 INSTANT    0.111000000E+03   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001030E+04
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 :  0.23791E+00 0.12472E+01
   Friction velocity        uet   :  0.14233E-01 0.72665E-01
   Friction velocity        uk    :  0.17431E-01 0.38735E-01
   Dimensionless distance   yplus :  0.42836E+03 0.95708E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64615E+01      57   0.13338E-02   0.21172E-01 
c  VelocityX    0.46297E+04      12   0.65229E-02   0.47553E-03 
c  VelocityY    0.46297E+04      12   0.65229E-02   0.25883E-04 
c  VelocityZ    0.46297E+04      12   0.65229E-02   0.55797E-04 
c  TurbEner     0.59738E+01      13   0.12737E-03   0.13839E-08 
c  Dissip       0.15665E+01      16   0.21117E-02   0.46736E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.93           54504           26774           27269
v  Velocity[x]            0.29266          2.0223         0.90805         0.90982
v  Velocity[y]           -0.36603         0.70043       0.0005845       0.0003609
v  Velocity[z]           -0.42248         0.50648      -0.0012771      -0.0013966
v  TurbEner             0.0010091        0.015433       0.0032836       0.0033433
v  Dissip              9.2071e-05        0.033918      0.00045251      0.00039101
v  TurbVisc               0.16484          11.343          4.7111          5.2724
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              111:        0.96742E-01

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


 INSTANT    0.112000000E+03   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002705E+04
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 :  0.23755E+00 0.13244E+01
   Friction velocity        uet   :  0.14212E-01 0.78954E-01
   Friction velocity        uk    :  0.17399E-01 0.38789E-01
   Dimensionless distance   yplus :  0.42798E+03 0.95709E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56021E+01      53   0.13775E-02   0.18373E-01 
c  VelocityX    0.46298E+04      12   0.65918E-02   0.34736E-03 
c  VelocityY    0.46298E+04      12   0.65918E-02   0.27229E-04 
c  VelocityZ    0.46298E+04      12   0.65918E-02   0.42304E-04 
c  TurbEner     0.59724E+01      13   0.16100E-03   0.22335E-08 
c  Dissip       0.15233E+01      17   0.26403E-02   0.90110E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.53           54509           26775           27269
v  Velocity[x]            0.29253          2.0961         0.90807         0.90984
v  Velocity[y]           -0.38227         0.69446      0.00057452      0.00035665
v  Velocity[z]           -0.42297         0.51107      -0.0012751      -0.0013917
v  TurbEner             0.0010091        0.014697       0.0032834       0.0033432
v  Dissip              9.2078e-05        0.032139      0.00045214      0.00039075
v  TurbVisc               0.16439          11.351          4.7111          5.2724
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              112:        0.95804E-01

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


 INSTANT    0.113000000E+03   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998852E+04
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 :  0.23761E+00 0.12151E+01
   Friction velocity        uet   :  0.14216E-01 0.72297E-01
   Friction velocity        uk    :  0.17399E-01 0.38806E-01
   Dimensionless distance   yplus :  0.42714E+03 0.95733E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61755E+01      53   0.14531E-02   0.20245E-01 
c  VelocityX    0.46296E+04      13   0.70782E-02   0.29640E-03 
c  VelocityY    0.46296E+04      13   0.70782E-02   0.31840E-04 
c  VelocityZ    0.46296E+04      13   0.70782E-02   0.35194E-04 
c  TurbEner     0.59727E+01      13   0.66805E-04   0.78086E-09 
c  Dissip       0.15239E+01      14   0.59710E-03   0.44516E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.53           54504           26775           27269
v  Velocity[x]            0.29285          2.1531         0.90804         0.90981
v  Velocity[y]           -0.36769         0.70257      0.00058949      0.00036676
v  Velocity[z]           -0.42018         0.50415      -0.0012612      -0.0013759
v  TurbEner             0.0010097        0.014542       0.0032833       0.0033431
v  Dissip              9.2037e-05         0.03173        0.000452      0.00039066
v  TurbVisc               0.16408          11.388          4.7111          5.2724
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              113:        0.95427E-01

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


 INSTANT    0.114000000E+03   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001026E+04
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 :  0.23733E+00 0.13250E+01
   Friction velocity        uet   :  0.14199E-01 0.78990E-01
   Friction velocity        uk    :  0.17404E-01 0.38803E-01
   Dimensionless distance   yplus :  0.42785E+03 0.95747E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66356E+01      62   0.14225E-02   0.21765E-01 
c  VelocityX    0.46297E+04      12   0.69522E-02   0.41328E-03 
c  VelocityY    0.46297E+04      12   0.69522E-02   0.36618E-04 
c  VelocityZ    0.46297E+04      12   0.69522E-02   0.44049E-04 
c  TurbEner     0.59725E+01      13   0.10274E-03   0.15089E-08 
c  Dissip       0.15261E+01      15   0.14156E-02   0.24742E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.19           54503           26776           27270
v  Velocity[x]            0.29264          1.9968         0.90807         0.90984
v  Velocity[y]           -0.38249         0.69235      0.00057379      0.00035324
v  Velocity[z]           -0.42066         0.51166      -0.0012844      -0.0014021
v  TurbEner             0.0010044        0.014973       0.0032833       0.0033431
v  Dissip              9.2042e-05         0.03274      0.00045203      0.00039068
v  TurbVisc               0.16447          11.369          4.7111          5.2724
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              114:        0.96422E-01

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


 INSTANT    0.115000000E+03   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997964E+04
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 :  0.23780E+00 0.12439E+01
   Friction velocity        uet   :  0.14229E-01 0.72670E-01
   Friction velocity        uk    :  0.17359E-01 0.38715E-01
   Dimensionless distance   yplus :  0.42706E+03 0.95731E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65267E+01      63   0.14454E-02   0.21390E-01 
c  VelocityX    0.46298E+04      12   0.71247E-02   0.38228E-03 
c  VelocityY    0.46298E+04      12   0.71247E-02   0.29050E-04 
c  VelocityZ    0.46298E+04      12   0.71247E-02   0.98368E-04 
c  TurbEner     0.59711E+01      13   0.13874E-03   0.18904E-08 
c  Dissip       0.14789E+01      17   0.27489E-02   0.97602E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.9           54513           26775           27269
v  Velocity[x]            0.29286          2.0851         0.90805         0.90982
v  Velocity[y]           -0.36657         0.70034      0.00058594      0.00036315
v  Velocity[z]           -0.42129         0.50603      -0.0012756      -0.0013967
v  TurbEner             0.0010057        0.014378        0.003283       0.0033429
v  Dissip              9.2029e-05        0.030979      0.00045162      0.00039039
v  TurbVisc               0.16382          11.369          4.7111          5.2724
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              115:        0.96667E-01

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


 INSTANT    0.116000000E+03   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001253E+04
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 :  0.23798E+00 0.13235E+01
   Friction velocity        uet   :  0.14240E-01 0.78899E-01
   Friction velocity        uk    :  0.17369E-01 0.38749E-01
   Dimensionless distance   yplus :  0.42653E+03 0.95749E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66113E+01      57   0.15635E-02   0.21672E-01 
c  VelocityX    0.46296E+04      12   0.67440E-02   0.39982E-03 
c  VelocityY    0.46296E+04      12   0.67440E-02   0.29170E-04 
c  VelocityZ    0.46296E+04      12   0.67440E-02   0.52322E-04 
c  TurbEner     0.59714E+01      13   0.70228E-04   0.92102E-09 
c  Dissip       0.14720E+01      14   0.83221E-03   0.78738E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -170           54502           26776           27270
v  Velocity[x]            0.29285          2.1347         0.90806         0.90984
v  Velocity[y]           -0.38221         0.69364      0.00058253      0.00036239
v  Velocity[z]           -0.42187         0.51115      -0.0012674      -0.0013846
v  TurbEner              0.001005        0.014288        0.003283       0.0033429
v  Dissip               9.207e-05        0.030417      0.00045145      0.00039028
v  TurbVisc               0.16374          11.342           4.711          5.2723
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              116:        0.96744E-01

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


 INSTANT    0.117000000E+03   TIME STEP NUMBER             117
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999183E+04
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 :  0.23759E+00 0.12162E+01
   Friction velocity        uet   :  0.14218E-01 0.72507E-01
   Friction velocity        uk    :  0.17364E-01 0.38789E-01
   Dimensionless distance   yplus :  0.42676E+03 0.95736E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62905E+01      55   0.13059E-02   0.20622E-01 
c  VelocityX    0.46298E+04      13   0.72628E-02   0.34760E-03 
c  VelocityY    0.46298E+04      13   0.72628E-02   0.41654E-04 
c  VelocityZ    0.46298E+04      13   0.72628E-02   0.32850E-04 
c  TurbEner     0.59717E+01      13   0.80792E-04   0.12297E-08 
c  Dissip       0.14813E+01      14   0.55226E-03   0.73353E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.31           54506           26775           27269
v  Velocity[x]            0.29264          2.1737         0.90805         0.90982
v  Velocity[y]             -0.367         0.70258      0.00058613       0.0003624
v  Velocity[z]           -0.42253         0.50473      -0.0012736      -0.0013932
v  TurbEner             0.0010021        0.014382       0.0032829       0.0033428
v  Dissip              9.2041e-05        0.030379      0.00045143      0.00039026
v  TurbVisc               0.16391          11.334           4.711          5.2723
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              117:        0.97122E-01

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


 INSTANT    0.118000000E+03   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001383E+04
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 :  0.23772E+00 0.13235E+01
   Friction velocity        uet   :  0.14226E-01 0.78893E-01
   Friction velocity        uk    :  0.17339E-01 0.38779E-01
   Dimensionless distance   yplus :  0.42650E+03 0.95713E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62410E+01      52   0.14610E-02   0.20463E-01 
c  VelocityX    0.46297E+04      12   0.68470E-02   0.36976E-03 
c  VelocityY    0.46297E+04      12   0.68470E-02   0.44925E-04 
c  VelocityZ    0.46297E+04      12   0.68470E-02   0.56123E-04 
c  TurbEner     0.59720E+01      13   0.13295E-03   0.13468E-08 
c  Dissip       0.14876E+01      15   0.18128E-02   0.31553E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.86           54507           26775           27270
v  Velocity[x]             0.2928           2.008         0.90805         0.90983
v  Velocity[y]           -0.38244         0.69465      0.00058292      0.00036113
v  Velocity[z]           -0.42208         0.51177      -0.0012734      -0.0013945
v  TurbEner             0.0010032        0.015031       0.0032828       0.0033427
v  Dissip              9.2064e-05        0.031777      0.00045145      0.00039028
v  TurbVisc               0.16364          11.362           4.711          5.2723
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              118:        0.95426E-01

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


 INSTANT    0.119000000E+03   TIME STEP NUMBER             119
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999184E+04
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 :  0.23786E+00 0.12257E+01
   Friction velocity        uet   :  0.14235E-01 0.72521E-01
   Friction velocity        uk    :  0.17348E-01 0.38772E-01
   Dimensionless distance   yplus :  0.42587E+03 0.95700E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60993E+01      52   0.14904E-02   0.19992E-01 
c  VelocityX    0.46297E+04      12   0.65567E-02   0.36513E-03 
c  VelocityY    0.46297E+04      12   0.65567E-02   0.30104E-04 
c  VelocityZ    0.46297E+04      12   0.65567E-02   0.40547E-04 
c  TurbEner     0.59707E+01      13   0.13783E-03   0.17938E-08 
c  Dissip       0.14443E+01      17   0.25835E-02   0.84044E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.79           54493           26775           27269
v  Velocity[x]            0.29306          2.0957         0.90805         0.90982
v  Velocity[y]           -0.36691         0.70135      0.00058591      0.00036638
v  Velocity[z]           -0.41975         0.50568      -0.0012607      -0.0013765
v  TurbEner             0.0010053        0.014402       0.0032826       0.0033426
v  Dissip              9.2142e-05        0.030071      0.00045107      0.00039003
v  TurbVisc               0.16343          11.325          4.7109          5.2722
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              119:        0.96359E-01

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


 INSTANT    0.120000000E+03   TIME STEP NUMBER             120
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001229E+04
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 :  0.23722E+00 0.13255E+01
   Friction velocity        uet   :  0.14197E-01 0.79005E-01
   Friction velocity        uk    :  0.17366E-01 0.38784E-01
   Dimensionless distance   yplus :  0.42680E+03 0.95727E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62345E+01      54   0.12838E-02   0.20437E-01 
c  VelocityX    0.46298E+04      13   0.70474E-02   0.32101E-03 
c  VelocityY    0.46298E+04      13   0.70474E-02   0.34366E-04 
c  VelocityZ    0.46298E+04      13   0.70474E-02   0.36561E-04 
c  TurbEner     0.59710E+01      13   0.73395E-04   0.10534E-08 
c  Dissip       0.14471E+01      14   0.36355E-03   0.23882E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.15           54498           26776           27270
v  Velocity[x]            0.29256          2.1482         0.90806         0.90984
v  Velocity[y]           -0.38286         0.69469      0.00056893      0.00035011
v  Velocity[z]           -0.42006         0.51049      -0.0012706      -0.0013919
v  TurbEner              0.001001         0.01439       0.0032826       0.0033425
v  Dissip              9.2178e-05        0.029877      0.00045091      0.00038991
v  TurbVisc               0.16392          11.327          4.7109          5.2722
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              120:        0.96698E-01

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


 INSTANT    0.121000000E+03   TIME STEP NUMBER             121
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998286E+04
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 :  0.23785E+00 0.12653E+01
   Friction velocity        uet   :  0.14236E-01 0.73627E-01
   Friction velocity        uk    :  0.17329E-01 0.38710E-01
   Dimensionless distance   yplus :  0.42622E+03 0.95706E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61800E+01      62   0.13612E-02   0.20253E-01 
c  VelocityX    0.46299E+04      13   0.70221E-02   0.36573E-03 
c  VelocityY    0.46299E+04      13   0.70221E-02   0.30213E-04 
c  VelocityZ    0.46299E+04      13   0.70221E-02   0.34467E-04 
c  TurbEner     0.59720E+01      12   0.83987E-04   0.82593E-09 
c  Dissip       0.14701E+01      15   0.85166E-03   0.15375E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.32           54517           26774           27268
v  Velocity[x]            0.29243          2.1787         0.90807         0.90984
v  Velocity[y]           -0.36739           0.703        0.000569      0.00034298
v  Velocity[z]           -0.42111         0.50429      -0.0012715      -0.0013891
v  TurbEner             0.0010034        0.014589       0.0032826       0.0033425
v  Dissip              9.2176e-05        0.030237      0.00045099      0.00038995
v  TurbVisc               0.16338          11.362           4.711          5.2723
v  total_pressure           83082      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              121:        0.96967E-01

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


 INSTANT    0.122000000E+03   TIME STEP NUMBER             122
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001769E+04
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 :  0.23800E+00 0.13248E+01
   Friction velocity        uet   :  0.14245E-01 0.78972E-01
   Friction velocity        uk    :  0.17350E-01 0.38754E-01
   Dimensionless distance   yplus :  0.42587E+03 0.95695E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61889E+01      52   0.12838E-02   0.20284E-01 
c  VelocityX    0.46298E+04      12   0.71288E-02   0.40225E-03 
c  VelocityY    0.46298E+04      12   0.71288E-02   0.27455E-04 
c  VelocityZ    0.46298E+04      12   0.71288E-02   0.71937E-04 
c  TurbEner     0.59729E+01      13   0.12525E-03   0.12225E-08 
c  Dissip       0.14825E+01      16   0.19830E-02   0.41425E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.51           54531           26775           27269
v  Velocity[x]            0.29324          2.0201         0.90807         0.90984
v  Velocity[y]           -0.38222          0.6939      0.00056958        0.000347
v  Velocity[z]            -0.4221          0.5118      -0.0012715      -0.0013914
v  TurbEner             0.0010038        0.015219       0.0032828       0.0033427
v  Dissip              9.2168e-05        0.031769      0.00045115      0.00039007
v  TurbVisc               0.16331          11.346           4.711          5.2723
v  total_pressure           83076      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              122:        0.95200E-01

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


 INSTANT    0.123000000E+03   TIME STEP NUMBER             123
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998611E+04
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 :  0.23736E+00 0.12155E+01
   Friction velocity        uet   :  0.14207E-01 0.72452E-01
   Friction velocity        uk    :  0.17353E-01 0.38794E-01
   Dimensionless distance   yplus :  0.42634E+03 0.95725E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54869E+01      53   0.12234E-02   0.17996E-01 
c  VelocityX    0.46297E+04      12   0.65023E-02   0.30839E-03 
c  VelocityY    0.46297E+04      12   0.65023E-02   0.43968E-04 
c  VelocityZ    0.46297E+04      12   0.65023E-02   0.10760E-03 
c  TurbEner     0.59720E+01      13   0.13027E-03   0.15988E-08 
c  Dissip       0.14514E+01      16   0.22968E-02   0.65193E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.79           54542           26775           27269
v  Velocity[x]            0.29267          2.0997         0.90805         0.90982
v  Velocity[y]           -0.36607         0.69944       0.0005735      0.00034883
v  Velocity[z]           -0.42102         0.50652      -0.0012597      -0.0013779
v  TurbEner             0.0010012        0.014624       0.0032827       0.0033426
v  Dissip              9.2174e-05        0.030193       0.0004509      0.00038989
v  TurbVisc               0.16354          11.348          4.7112          5.2725
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              123:        0.94823E-01

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


 INSTANT    0.124000000E+03   TIME STEP NUMBER             124
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000064E+04
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 :  0.23797E+00 0.13240E+01
   Friction velocity        uet   :  0.14244E-01 0.78919E-01
   Friction velocity        uk    :  0.17331E-01 0.38834E-01
   Dimensionless distance   yplus :  0.42609E+03 0.95677E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58568E+01      57   0.12049E-02   0.19198E-01 
c  VelocityX    0.46297E+04      12   0.72123E-02   0.34133E-03 
c  VelocityY    0.46297E+04      12   0.72123E-02   0.28294E-04 
c  VelocityZ    0.46297E+04      12   0.72123E-02   0.40488E-04 
c  TurbEner     0.59727E+01      12   0.58544E-04   0.63406E-09 
c  Dissip       0.14562E+01      13   0.27802E-03   0.20823E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.42           54550           26776           27270
v  Velocity[x]            0.29244          2.1479         0.90805         0.90983
v  Velocity[y]           -0.38236         0.69062      0.00057046      0.00034875
v  Velocity[z]           -0.42203         0.51104        -0.00126      -0.0013817
v  TurbEner             0.0010026        0.014663       0.0032828       0.0033427
v  Dissip              9.2157e-05        0.030196      0.00045087      0.00038987
v  TurbVisc               0.16326          11.325          4.7112          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              124:        0.96013E-01

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


 INSTANT    0.125000000E+03   TIME STEP NUMBER             125
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399996847E+04
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 :  0.23772E+00 0.12426E+01
   Friction velocity        uet   :  0.14229E-01 0.72386E-01
   Friction velocity        uk    :  0.17343E-01 0.38815E-01
   Dimensionless distance   yplus :  0.42548E+03 0.95655E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60753E+01      53   0.13906E-02   0.19908E-01 
c  VelocityX    0.46298E+04      12   0.75917E-02   0.41204E-03 
c  VelocityY    0.46298E+04      12   0.75917E-02   0.31093E-04 
c  VelocityZ    0.46298E+04      12   0.75917E-02   0.48315E-04 
c  TurbEner     0.59739E+01      13   0.90265E-04   0.11515E-08 
c  Dissip       0.14804E+01      15   0.87944E-03   0.17610E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.67           54542           26776           27270
v  Velocity[x]            0.29299          2.1858         0.90806         0.90984
v  Velocity[y]           -0.36779         0.69933      0.00057523      0.00035424
v  Velocity[z]           -0.41997         0.50416      -0.0012626      -0.0013797
v  TurbEner              0.001005        0.014775        0.003283       0.0033429
v  Dissip              9.2099e-05        0.030528      0.00045108      0.00039002
v  TurbVisc               0.16301          11.318          4.7113          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              125:        0.94900E-01

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


 INSTANT    0.126000000E+03   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998051E+04
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 :  0.23737E+00 0.13219E+01
   Friction velocity        uet   :  0.14208E-01 0.78799E-01
   Friction velocity        uk    :  0.17364E-01 0.38715E-01
   Dimensionless distance   yplus :  0.42650E+03 0.95686E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63850E+01      59   0.16150E-02   0.20947E-01 
c  VelocityX    0.46299E+04      12   0.69454E-02   0.36794E-03 
c  VelocityY    0.46299E+04      12   0.69454E-02   0.26940E-04 
c  VelocityZ    0.46299E+04      12   0.69454E-02   0.37454E-04 
c  TurbEner     0.59756E+01      13   0.89668E-04   0.13178E-08 
c  Dissip       0.15133E+01      15   0.11444E-02   0.22735E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.17           54518           26777           27271
v  Velocity[x]            0.29269          2.2119         0.90807         0.90985
v  Velocity[y]           -0.38255         0.69225      0.00057445      0.00035827
v  Velocity[z]           -0.42039         0.51171      -0.0012481      -0.0013687
v  TurbEner             0.0010009        0.014997       0.0032832       0.0033431
v  Dissip              9.2038e-05        0.031268      0.00045139      0.00039025
v  TurbVisc               0.16357          11.345          4.7114          5.2726
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              126:        0.97853E-01

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


 INSTANT    0.127000000E+03   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999320E+04
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 :  0.23784E+00 0.12146E+01
   Friction velocity        uet   :  0.14237E-01 0.72407E-01
   Friction velocity        uk    :  0.17328E-01 0.38648E-01
   Dimensionless distance   yplus :  0.42602E+03 0.95657E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60220E+01      59   0.13818E-02   0.19747E-01 
c  VelocityX    0.46298E+04      12   0.66838E-02   0.38327E-03 
c  VelocityY    0.46298E+04      12   0.66838E-02   0.30572E-04 
c  VelocityZ    0.46298E+04      12   0.66838E-02   0.34274E-04 
c  TurbEner     0.59751E+01      13   0.12665E-03   0.16787E-08 
c  Dissip       0.15344E+01      16   0.22509E-02   0.58026E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.28           54525           26776           27270
v  Velocity[x]             0.2928          2.0343         0.90804         0.90981
v  Velocity[y]           -0.36651         0.69916      0.00058229      0.00035923
v  Velocity[z]           -0.42287         0.50605       -0.001268      -0.0013865
v  TurbEner             0.0010033        0.015608       0.0032833       0.0033432
v  Dissip              9.2026e-05        0.033046      0.00045167      0.00039045
v  TurbVisc               0.16312          11.396          4.7114          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              127:        0.96929E-01

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


 INSTANT    0.128000000E+03   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002136E+04
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 :  0.23761E+00 0.13240E+01
   Friction velocity        uet   :  0.14223E-01 0.78928E-01
   Friction velocity        uk    :  0.17349E-01 0.38711E-01
   Dimensionless distance   yplus :  0.42575E+03 0.95649E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64194E+01      57   0.14270E-02   0.21057E-01 
c  VelocityX    0.46297E+04      12   0.68930E-02   0.47081E-03 
c  VelocityY    0.46297E+04      12   0.68930E-02   0.41807E-04 
c  VelocityZ    0.46297E+04      12   0.68930E-02   0.59823E-04 
c  TurbEner     0.59729E+01      14   0.11539E-03   0.18772E-08 
c  Dissip       0.14872E+01      16   0.15585E-02   0.59330E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.07           54523           26776           27270
v  Velocity[x]            0.29277          1.7302         0.90804         0.90981
v  Velocity[y]            -0.3822         0.69291      0.00056258       0.0003471
v  Velocity[z]           -0.41961         0.51114      -0.0012699      -0.0013863
v  TurbEner             0.0010034        0.015469       0.0032832       0.0033431
v  Dissip              9.2015e-05        0.032966       0.0004515      0.00039035
v  TurbVisc                0.1631          11.386          4.7114          5.2727
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              128:        0.95410E-01

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


 INSTANT    0.129000000E+03   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000396E+04
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 :  0.23760E+00 0.12361E+01
   Friction velocity        uet   :  0.14222E-01 0.72274E-01
   Friction velocity        uk    :  0.17350E-01 0.38756E-01
   Dimensionless distance   yplus :  0.42621E+03 0.95701E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64374E+01      59   0.15262E-02   0.21108E-01 
c  VelocityX    0.46298E+04      13   0.70623E-02   0.41039E-03 
c  VelocityY    0.46298E+04      13   0.70623E-02   0.24327E-04 
c  VelocityZ    0.46298E+04      13   0.70623E-02   0.47156E-04 
c  TurbEner     0.59683E+01      15   0.40131E-03   0.80694E-08 
c  Dissip       0.13399E+01      18   0.81701E-02   0.46922E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.36           54504           26775           27269
v  Velocity[x]            0.29266          1.8772         0.90806         0.90983
v  Velocity[y]           -0.36695         0.70182      0.00056939      0.00034983
v  Velocity[z]           -0.42116         0.50476      -0.0012695      -0.0013859
v  TurbEner              0.001001        0.013325       0.0032828       0.0033427
v  Dissip              9.2021e-05         0.02735      0.00045082      0.00038983
v  TurbVisc                0.1634          11.333          4.7114          5.2727
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              129:        0.97468E-01

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


 INSTANT    0.130000000E+03   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002401E+04
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 :  0.23773E+00 0.13245E+01
   Friction velocity        uet   :  0.14230E-01 0.78954E-01
   Friction velocity        uk    :  0.17329E-01 0.38761E-01
   Dimensionless distance   yplus :  0.42611E+03 0.95736E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66448E+01      67   0.13822E-02   0.21782E-01 
c  VelocityX    0.46299E+04      12   0.67833E-02   0.41241E-03 
c  VelocityY    0.46299E+04      12   0.67833E-02   0.30583E-04 
c  VelocityZ    0.46299E+04      12   0.67833E-02   0.81973E-04 
c  TurbEner     0.59665E+01      14   0.15490E-03   0.27570E-08 
c  Dissip       0.12853E+01      18   0.38590E-02   0.13674E-07 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.94           54510           26775           27270
v  Velocity[x]            0.29302          2.0068         0.90805         0.90982
v  Velocity[y]           -0.38237         0.69159      0.00057572      0.00035627
v  Velocity[z]           -0.42093         0.51172       -0.001264      -0.0013851
v  TurbEner             0.0010025        0.012607       0.0032825       0.0033425
v  Dissip              9.2008e-05        0.024927      0.00045014      0.00038934
v  TurbVisc               0.16325          11.321          4.7113          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              130:        0.98640E-01

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


 INSTANT    0.131000000E+03   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998738E+04
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 :  0.23814E+00 0.12167E+01
   Friction velocity        uet   :  0.14254E-01 0.72526E-01
   Friction velocity        uk    :  0.17342E-01 0.38748E-01
   Dimensionless distance   yplus :  0.42563E+03 0.95709E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71578E+01      55   0.15467E-02   0.23471E-01 
c  VelocityX    0.46298E+04      12   0.68138E-02   0.37163E-03 
c  VelocityY    0.46298E+04      12   0.68138E-02   0.35701E-04 
c  VelocityZ    0.46298E+04      12   0.68138E-02   0.39636E-04 
c  TurbEner     0.59661E+01      13   0.88074E-04   0.13829E-08 
c  Dissip       0.12491E+01      17   0.22912E-02   0.81265E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.58           54517           26775           27270
v  Velocity[x]             0.2929          2.0689         0.90805         0.90983
v  Velocity[y]           -0.36681         0.70033      0.00056973      0.00034867
v  Velocity[z]           -0.42142         0.50578      -0.0012691      -0.0013855
v  TurbEner             0.0010054        0.012595       0.0032823       0.0033423
v  Dissip              9.2042e-05        0.024008      0.00044947      0.00038887
v  TurbVisc               0.16317           11.35          4.7115          5.2728
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              131:        0.95467E-01

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


 INSTANT    0.132000000E+03   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999193E+04
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 :  0.23758E+00 0.13238E+01
   Friction velocity        uet   :  0.14220E-01 0.78902E-01
   Friction velocity        uk    :  0.17368E-01 0.38740E-01
   Dimensionless distance   yplus :  0.42675E+03 0.95750E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66093E+01      56   0.14788E-02   0.21680E-01 
c  VelocityX    0.46299E+04      12   0.66238E-02   0.37000E-03 
c  VelocityY    0.46299E+04      12   0.66238E-02   0.45663E-04 
c  VelocityZ    0.46299E+04      12   0.66238E-02   0.31379E-04 
c  TurbEner     0.59666E+01      13   0.74331E-04   0.10543E-08 
c  Dissip       0.12410E+01      17   0.95024E-03   0.19223E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.26           54503           26776           27270
v  Velocity[x]            0.29266          2.1358         0.90806         0.90983
v  Velocity[y]           -0.38288         0.69308      0.00057588      0.00035892
v  Velocity[z]           -0.42315         0.51047      -0.0012559      -0.0013736
v  TurbEner             0.0010025        0.012802       0.0032821       0.0033422
v  Dissip              9.2099e-05        0.023792      0.00044894      0.00038849
v  TurbVisc               0.16388          11.333          4.7117           5.273
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              132:        0.95777E-01

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


 INSTANT    0.133000000E+03   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998443E+04
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 :  0.23756E+00 0.12165E+01
   Friction velocity        uet   :  0.14218E-01 0.72520E-01
   Friction velocity        uk    :  0.17342E-01 0.38632E-01
   Dimensionless distance   yplus :  0.42641E+03 0.95772E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64255E+01      56   0.12278E-02   0.21058E-01 
c  VelocityX    0.46299E+04      13   0.76545E-02   0.34875E-03 
c  VelocityY    0.46299E+04      13   0.76545E-02   0.32200E-04 
c  VelocityZ    0.46299E+04      13   0.76545E-02   0.44835E-04 
c  TurbEner     0.59670E+01      13   0.10200E-03   0.16313E-08 
c  Dissip       0.12495E+01      16   0.70351E-03   0.82763E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.42           54508           26775           27270
v  Velocity[x]            0.29274          2.1615         0.90806         0.90983
v  Velocity[y]            -0.3674         0.70185      0.00057247      0.00034903
v  Velocity[z]           -0.42205         0.50429      -0.0012683      -0.0013846
v  TurbEner             0.0010062        0.013257        0.003282        0.003342
v  Dissip              9.2135e-05        0.024221      0.00044856      0.00038821
v  TurbVisc               0.16368          11.331          4.7118          5.2731
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              133:        0.96051E-01

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


 INSTANT    0.134000000E+03   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002456E+04
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 :  0.23788E+00 0.13239E+01
   Friction velocity        uet   :  0.14235E-01 0.78912E-01
   Friction velocity        uk    :  0.17374E-01 0.38715E-01
   Dimensionless distance   yplus :  0.42635E+03 0.95723E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71020E+01      65   0.15279E-02   0.23277E-01 
c  VelocityX    0.46299E+04      12   0.69493E-02   0.42855E-03 
c  VelocityY    0.46299E+04      12   0.69493E-02   0.40962E-04 
c  VelocityZ    0.46299E+04      12   0.69493E-02   0.12139E-03 
c  TurbEner     0.59685E+01      14   0.15116E-03   0.23106E-08 
c  Dissip       0.12662E+01      16   0.20047E-02   0.39139E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.16           54515           26776           27270
v  Velocity[x]            0.29295          2.0119         0.90804         0.90982
v  Velocity[y]            -0.3823         0.69474      0.00058369      0.00036305
v  Velocity[z]           -0.42026         0.51187      -0.0012557      -0.0013768
v  TurbEner             0.0010075        0.014088       0.0032821       0.0033421
v  Dissip              9.2133e-05        0.025713      0.00044845      0.00038814
v  TurbVisc               0.16377          11.357           4.712          5.2732
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              134:        0.98211E-01

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


 INSTANT    0.135000000E+03   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998916E+04
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 :  0.23729E+00 0.12169E+01
   Friction velocity        uet   :  0.14199E-01 0.72543E-01
   Friction velocity        uk    :  0.17386E-01 0.38795E-01
   Dimensionless distance   yplus :  0.42707E+03 0.95671E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63006E+01      66   0.15604E-02   0.20679E-01 
c  VelocityX    0.46299E+04      12   0.66169E-02   0.38861E-03 
c  VelocityY    0.46299E+04      12   0.66169E-02   0.36700E-04 
c  VelocityZ    0.46299E+04      12   0.66169E-02   0.56377E-04 
c  TurbEner     0.59682E+01      13   0.87877E-04   0.12342E-08 
c  Dissip       0.12469E+01      16   0.14608E-02   0.29712E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.79           54507           26776           27271
v  Velocity[x]            0.29276          2.0889         0.90806         0.90984
v  Velocity[y]           -0.36613         0.70141      0.00058415       0.0003629
v  Velocity[z]           -0.42161         0.50648      -0.0012602      -0.0013772
v  TurbEner             0.0010053        0.013782       0.0032821       0.0033421
v  Dissip              9.2134e-05         0.02481      0.00044806      0.00038789
v  TurbVisc               0.16422          11.337          4.7122          5.2734
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              135:        0.98376E-01

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


 INSTANT    0.136000000E+03   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999709E+04
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 :  0.23759E+00 0.13255E+01
   Friction velocity        uet   :  0.14216E-01 0.79004E-01
   Friction velocity        uk    :  0.17367E-01 0.38794E-01
   Dimensionless distance   yplus :  0.42703E+03 0.95651E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62208E+01      53   0.12525E-02   0.20388E-01 
c  VelocityX    0.46300E+04      13   0.70679E-02   0.37047E-03 
c  VelocityY    0.46300E+04      13   0.70679E-02   0.24855E-04 
c  VelocityZ    0.46300E+04      13   0.70679E-02   0.33331E-04 
c  TurbEner     0.59687E+01      13   0.77565E-04   0.10954E-08 
c  Dissip       0.12598E+01      15   0.53625E-03   0.68416E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.23           54507           26777           27271
v  Velocity[x]            0.29251          2.1455         0.90805         0.90982
v  Velocity[y]            -0.3823         0.69542      0.00057728      0.00035886
v  Velocity[z]           -0.42184         0.51115       -0.001259      -0.0013793
v  TurbEner             0.0010062        0.013919       0.0032822       0.0033422
v  Dissip              9.2121e-05        0.024981      0.00044795      0.00038781
v  TurbVisc               0.16414          11.343          4.7124          5.2736
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              136:        0.95938E-01

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


 INSTANT    0.137000000E+03   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999202E+04
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 :  0.23798E+00 0.12142E+01
   Friction velocity        uet   :  0.14238E-01 0.72324E-01
   Friction velocity        uk    :  0.17374E-01 0.38759E-01
   Dimensionless distance   yplus :  0.42643E+03 0.95620E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53976E+01      53   0.14150E-02   0.17695E-01 
c  VelocityX    0.46300E+04      13   0.71328E-02   0.35619E-03 
c  VelocityY    0.46300E+04      13   0.71328E-02   0.24010E-04 
c  VelocityZ    0.46300E+04      13   0.71328E-02   0.42441E-04 
c  TurbEner     0.59698E+01      13   0.12672E-03   0.17271E-08 
c  Dissip       0.12773E+01      16   0.18399E-02   0.41129E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.03           54517           26776           27270
v  Velocity[x]            0.29294           1.993         0.90806         0.90983
v  Velocity[y]           -0.36775         0.70323      0.00057499      0.00035283
v  Velocity[z]           -0.42207          0.5042      -0.0012707      -0.0013876
v  TurbEner             0.0010068         0.01453       0.0032825       0.0033424
v  Dissip              9.2106e-05        0.026298      0.00044807      0.00038791
v  TurbVisc               0.16389          11.382          4.7127          5.2739
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              137:        0.95994E-01

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


 INSTANT    0.138000000E+03   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001310E+04
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 :  0.23762E+00 0.13258E+01
   Friction velocity        uet   :  0.14216E-01 0.79029E-01
   Friction velocity        uk    :  0.17379E-01 0.38749E-01
   Dimensionless distance   yplus :  0.42716E+03 0.95616E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63127E+01      58   0.15167E-02   0.20707E-01 
c  VelocityX    0.46300E+04      12   0.66593E-02   0.37312E-03 
c  VelocityY    0.46300E+04      12   0.66593E-02   0.29856E-04 
c  VelocityZ    0.46300E+04      12   0.66593E-02   0.10777E-03 
c  TurbEner     0.59696E+01      13   0.98591E-04   0.14489E-08 
c  Dissip       0.12589E+01      16   0.15252E-02   0.32954E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.77           54507           26777           27271
v  Velocity[x]            0.29275          2.0731         0.90806         0.90983
v  Velocity[y]           -0.38247         0.69266      0.00057609       0.0003576
v  Velocity[z]           -0.42089         0.51169      -0.0012517      -0.0013748
v  TurbEner             0.0010018        0.014102       0.0032827       0.0033426
v  Dissip               9.208e-05        0.025345      0.00044791      0.00038781
v  TurbVisc               0.16436          11.344          4.7129          5.2741
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              138:        0.95933E-01

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


 INSTANT    0.139000000E+03   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998568E+04
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 :  0.23800E+00 0.12178E+01
   Friction velocity        uet   :  0.14239E-01 0.72591E-01
   Friction velocity        uk    :  0.17336E-01 0.38725E-01
   Dimensionless distance   yplus :  0.42650E+03 0.95586E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58407E+01      55   0.12613E-02   0.19152E-01 
c  VelocityX    0.46301E+04      12   0.67485E-02   0.36504E-03 
c  VelocityY    0.46301E+04      12   0.67485E-02   0.25453E-04 
c  VelocityZ    0.46301E+04      12   0.67485E-02   0.49788E-04 
c  TurbEner     0.59698E+01      12   0.71101E-04   0.91666E-09 
c  Dissip       0.12701E+01      15   0.53979E-03   0.71441E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.06           54508           26777           27271
v  Velocity[x]            0.29286          2.1294         0.90806         0.90983
v  Velocity[y]           -0.36658         0.69996      0.00056888      0.00034501
v  Velocity[z]            -0.4225          0.5061       -0.001267       -0.001384
v  TurbEner             0.0010036        0.014127       0.0032828       0.0033427
v  Dissip              9.2094e-05        0.025363      0.00044793      0.00038781
v  TurbVisc               0.16398          11.336          4.7132          5.2744
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              139:        0.95695E-01

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


 INSTANT    0.140000000E+03   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999494E+04
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 :  0.23765E+00 0.13242E+01
   Friction velocity        uet   :  0.14218E-01 0.78927E-01
   Friction velocity        uk    :  0.17352E-01 0.38787E-01
   Dimensionless distance   yplus :  0.42615E+03 0.95576E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58099E+01      55   0.13553E-02   0.19042E-01 
c  VelocityX    0.46301E+04      12   0.71613E-02   0.33549E-03 
c  VelocityY    0.46301E+04      12   0.71613E-02   0.21156E-04 
c  VelocityZ    0.46301E+04      12   0.71613E-02   0.32409E-04 
c  TurbEner     0.59717E+01      13   0.84561E-04   0.10529E-08 
c  Dissip       0.12961E+01      16   0.98102E-03   0.20061E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.86           54514           26777           27271
v  Velocity[x]            0.29283          2.1716         0.90805         0.90983
v  Velocity[y]           -0.38225         0.69298      0.00057019      0.00034971
v  Velocity[z]           -0.42062         0.51111      -0.0012638      -0.0013835
v  TurbEner             0.0010041        0.014312       0.0032832        0.003343
v  Dissip              9.2108e-05        0.025808      0.00044817      0.00038797
v  TurbVisc               0.16403          11.363          4.7134          5.2746
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              140:        0.95269E-01

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


 INSTANT    0.141000000E+03   TIME STEP NUMBER             141
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999323E+04
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 :  0.23725E+00 0.12163E+01
   Friction velocity        uet   :  0.14194E-01 0.72501E-01
   Friction velocity        uk    :  0.17356E-01 0.38814E-01
   Dimensionless distance   yplus :  0.42667E+03 0.95593E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63358E+01      63   0.15893E-02   0.20788E-01 
c  VelocityX    0.46302E+04      13   0.68968E-02   0.41148E-03 
c  VelocityY    0.46302E+04      13   0.68968E-02   0.23387E-04 
c  VelocityZ    0.46302E+04      13   0.68968E-02   0.51033E-04 
c  TurbEner     0.59727E+01      13   0.12062E-03   0.18898E-08 
c  Dissip       0.13157E+01      16   0.20093E-02   0.48672E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.36           54504           26777           27272
v  Velocity[x]            0.29269          2.0061         0.90808         0.90985
v  Velocity[y]           -0.36702         0.70204      0.00057612      0.00035373
v  Velocity[z]           -0.42082         0.50477       -0.001271      -0.0013874
v  TurbEner             0.0010021        0.014958       0.0032836       0.0033433
v  Dissip              9.2061e-05        0.027323       0.0004485      0.00038821
v  TurbVisc               0.16452          11.347          4.7138          5.2749
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              141:        0.96961E-01

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


 INSTANT    0.142000000E+03   TIME STEP NUMBER             142
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999932E+04
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 :  0.23777E+00 0.13235E+01
   Friction velocity        uet   :  0.14226E-01 0.78883E-01
   Friction velocity        uk    :  0.17339E-01 0.38796E-01
   Dimensionless distance   yplus :  0.42657E+03 0.95623E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62743E+01      62   0.13649E-02   0.20571E-01 
c  VelocityX    0.46302E+04      12   0.71305E-02   0.35066E-03 
c  VelocityY    0.46302E+04      12   0.71305E-02   0.64768E-04 
c  VelocityZ    0.46302E+04      12   0.71305E-02   0.13599E-03 
c  TurbEner     0.59718E+01      13   0.10484E-03   0.18632E-08 
c  Dissip       0.12982E+01      16   0.15660E-02   0.40207E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.12           54525           26778           27272
v  Velocity[x]            0.29285          2.0837         0.90805         0.90983
v  Velocity[y]           -0.38245         0.69438       0.0005783      0.00035511
v  Velocity[z]           -0.42253         0.51176      -0.0012596      -0.0013798
v  TurbEner             0.0010054        0.014512       0.0032837       0.0033434
v  Dissip              9.2055e-05        0.026403       0.0004484      0.00038813
v  TurbVisc               0.16461          11.355          4.7141          5.2752
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              142:        0.95934E-01

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


 INSTANT    0.143000000E+03   TIME STEP NUMBER             143
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999119E+04
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 :  0.23791E+00 0.12169E+01
   Friction velocity        uet   :  0.14235E-01 0.72545E-01
   Friction velocity        uk    :  0.17367E-01 0.38791E-01
   Dimensionless distance   yplus :  0.42623E+03 0.95581E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64980E+01      56   0.13901E-02   0.21311E-01 
c  VelocityX    0.46302E+04      12   0.71876E-02   0.41379E-03 
c  VelocityY    0.46302E+04      12   0.71876E-02   0.30419E-04 
c  VelocityZ    0.46302E+04      12   0.71876E-02   0.57808E-04 
c  TurbEner     0.59728E+01      13   0.66646E-04   0.72189E-09 
c  Dissip       0.13127E+01      15   0.56501E-03   0.82526E-09 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.52           54517           26778           27272
v  Velocity[x]            0.29307          2.1347         0.90808         0.90985
v  Velocity[y]            -0.3669         0.70046      0.00056909      0.00034447
v  Velocity[z]            -0.4204         0.50568      -0.0012697      -0.0013871
v  TurbEner             0.0010104        0.014552        0.003284       0.0033436
v  Dissip              9.2057e-05        0.026515      0.00044855      0.00038822
v  TurbVisc               0.16472          11.393          4.7143          5.2754
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              143:        0.95632E-01

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


 INSTANT    0.144000000E+03   TIME STEP NUMBER             144
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000536E+04
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 :  0.23799E+00 0.13256E+01
   Friction velocity        uet   :  0.14240E-01 0.79016E-01
   Friction velocity        uk    :  0.17410E-01 0.38819E-01
   Dimensionless distance   yplus :  0.42767E+03 0.95590E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59621E+01      56   0.14729E-02   0.19556E-01 
c  VelocityX    0.46304E+04      12   0.65322E-02   0.36684E-03 
c  VelocityY    0.46304E+04      12   0.65322E-02   0.24773E-04 
c  VelocityZ    0.46304E+04      12   0.65322E-02   0.32900E-04 
c  TurbEner     0.59746E+01      13   0.81278E-04   0.13021E-08 
c  Dissip       0.13402E+01      16   0.10485E-02   0.23778E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.62           54512           26778           27272
v  Velocity[x]            0.29258          2.1758         0.90807         0.90985
v  Velocity[y]            -0.3829         0.69381      0.00057089      0.00035163
v  Velocity[z]           -0.42188         0.51049      -0.0012583      -0.0013792
v  TurbEner               0.00101        0.014708       0.0032845        0.003344
v  Dissip              9.2083e-05        0.027025      0.00044888      0.00038845
v  TurbVisc               0.16574          11.372          4.7146          5.2757
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              144:        0.95823E-01

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


 INSTANT    0.145000000E+03   TIME STEP NUMBER             145
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998350E+04
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 :  0.23767E+00 0.12138E+01
   Friction velocity        uet   :  0.14222E-01 0.72295E-01
   Friction velocity        uk    :  0.17407E-01 0.38768E-01
   Dimensionless distance   yplus :  0.42776E+03 0.95617E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58093E+01      57   0.13884E-02   0.19053E-01 
c  VelocityX    0.46303E+04      13   0.71752E-02   0.37204E-03 
c  VelocityY    0.46303E+04      13   0.71752E-02   0.28516E-04 
c  VelocityZ    0.46303E+04      13   0.71752E-02   0.33896E-04 
c  TurbEner     0.59750E+01      13   0.11916E-03   0.17672E-08 
c  Dissip       0.13623E+01      16   0.20887E-02   0.52379E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.48           54510           26778           27272
v  Velocity[x]            0.29248          2.0102         0.90805         0.90982
v  Velocity[y]           -0.36742         0.70222      0.00057624      0.00035136
v  Velocity[z]           -0.42259         0.50435       -0.001274      -0.0013921
v  TurbEner             0.0010162        0.015324       0.0032851       0.0033444
v  Dissip              9.2037e-05        0.028653      0.00044927      0.00038872
v  TurbVisc               0.16587          11.372          4.7149           5.276
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              145:        0.96621E-01

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


 INSTANT    0.146000000E+03   TIME STEP NUMBER             146
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000995E+04
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 :  0.23760E+00 0.13248E+01
   Friction velocity        uet   :  0.14218E-01 0.78971E-01
   Friction velocity        uk    :  0.17460E-01 0.38775E-01
   Dimensionless distance   yplus :  0.42817E+03 0.95576E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68216E+01      53   0.14795E-02   0.22368E-01 
c  VelocityX    0.46303E+04      12   0.74955E-02   0.40643E-03 
c  VelocityY    0.46303E+04      12   0.74955E-02   0.33941E-04 
c  VelocityZ    0.46303E+04      12   0.74955E-02   0.61196E-04 
c  TurbEner     0.59745E+01      13   0.11367E-03   0.16968E-08 
c  Dissip       0.13417E+01      16   0.15973E-02   0.42229E-08 
---------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.12           54515           26778           27272
v  Velocity[x]            0.29296          2.0815         0.90807         0.90985
v  Velocity[y]           -0.38222         0.69322      0.00056437      0.00034408
v  Velocity[z]            -0.4196         0.51191      -0.0012637      -0.0013819
v  TurbEner             0.0010199        0.014805       0.0032853       0.0033446
v  Dissip              9.2054e-05        0.027692      0.00044928      0.00038873
v  TurbVisc               0.16629          11.344          4.7152          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              146:        0.95621E-01

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


 INSTANT    0.147000000E+03   TIME STEP NUMBER             147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999906E+04
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 :  0.23753E+00 0.12155E+01
   Friction velocity        uet   :  0.14215E-01 0.72453E-01
   Friction velocity        uk    :  0.17492E-01 0.38810E-01
   Dimensionless distance   yplus :  0.42930E+03 0.95581E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64010E+01      55   0.14613E-02   0.21000E-01 
c  VelocityX    0.46304E+04      12   0.61750E-02   0.37515E-03 
c  VelocityY    0.46304E+04      12   0.61750E-02   0.38075E-04 
c  VelocityZ    0.46304E+04      12   0.61750E-02   0.10056E-03 
c  TurbEner     0.59752E+01      13   0.74136E-04   0.96508E-09 
c  Dissip       0.13575E+01      14   0.44197E-03   0.51300E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.43           54522           26777           27272
v  Velocity[x]            0.29274          2.1415         0.90807         0.90985
v  Velocity[y]           -0.36603         0.69901      0.00057832       0.0003551
v  Velocity[z]           -0.42068         0.50663      -0.0012485      -0.0013666
v  TurbEner             0.0010211        0.014746       0.0032856       0.0033448
v  Dissip              9.2029e-05        0.027635      0.00044946      0.00038886
v  TurbVisc               0.16705          11.336          4.7154          5.2765
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              147:        0.95576E-01

===============================================================


 INSTANT    0.148000000E+03   TIME STEP NUMBER             148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002383E+04
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 :  0.23765E+00 0.13242E+01
   Friction velocity        uet   :  0.14223E-01 0.78935E-01
   Friction velocity        uk    :  0.17502E-01 0.38807E-01
   Dimensionless distance   yplus :  0.42990E+03 0.95629E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.52334E+01      50   0.10904E-02   0.17165E-01 
c  VelocityX    0.46304E+04      12   0.71313E-02   0.30835E-03 
c  VelocityY    0.46304E+04      12   0.71313E-02   0.27224E-04 
c  VelocityZ    0.46304E+04      12   0.71313E-02   0.41136E-04 
c  TurbEner     0.59761E+01      13   0.84469E-04   0.11695E-08 
c  Dissip       0.13833E+01      16   0.11056E-02   0.25179E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.92           54523           26778           27272
v  Velocity[x]            0.29255          2.1697         0.90805         0.90983
v  Velocity[y]           -0.38232         0.69073      0.00057508      0.00035235
v  Velocity[z]           -0.42115         0.51112       -0.001257      -0.0013787
v  TurbEner             0.0010257         0.01497       0.0032859       0.0033451
v  Dissip              9.2055e-05         0.02824      0.00044977      0.00038906
v  TurbVisc                0.1674          11.365          4.7156          5.2766
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              148:        0.95058E-01

===============================================================


 INSTANT    0.149000000E+03   TIME STEP NUMBER             149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998534E+04
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 :  0.23809E+00 0.12187E+01
   Friction velocity        uet   :  0.14250E-01 0.72407E-01
   Friction velocity        uk    :  0.17542E-01 0.38838E-01
   Dimensionless distance   yplus :  0.43004E+03 0.95589E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59131E+01      50   0.12502E-02   0.19383E-01 
c  VelocityX    0.46304E+04      12   0.74774E-02   0.32504E-03 
c  VelocityY    0.46304E+04      12   0.74774E-02   0.23779E-04 
c  VelocityZ    0.46304E+04      12   0.74774E-02   0.45629E-04 
c  TurbEner     0.59774E+01      13   0.73144E-04   0.89709E-09 
c  Dissip       0.14151E+01      16   0.11768E-02   0.27098E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.87           54518           26778           27272
v  Velocity[x]            0.29293          2.1939         0.90806         0.90984
v  Velocity[y]           -0.36776         0.70007      0.00056952      0.00034494
v  Velocity[z]            -0.4216         0.50418      -0.0012625      -0.0013831
v  TurbEner             0.0010309        0.015182       0.0032862       0.0033453
v  Dissip              9.2067e-05        0.028947       0.0004502      0.00038935
v  TurbVisc               0.16762          11.341          4.7158          5.2769
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              149:        0.94804E-01

===============================================================


 INSTANT    0.150000000E+03   TIME STEP NUMBER             150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999276E+04
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 :  0.23757E+00 0.13219E+01
   Friction velocity        uet   :  0.14219E-01 0.78803E-01
   Friction velocity        uk    :  0.17586E-01 0.38862E-01
   Dimensionless distance   yplus :  0.43167E+03 0.95580E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70794E+01      54   0.16955E-02   0.23228E-01 
c  VelocityX    0.46304E+04      12   0.74212E-02   0.39230E-03 
c  VelocityY    0.46304E+04      12   0.74212E-02   0.53729E-04 
c  VelocityZ    0.46304E+04      12   0.74212E-02   0.52840E-04 
c  TurbEner     0.59785E+01      13   0.13643E-03   0.17463E-08 
c  Dissip       0.14431E+01      16   0.24445E-02   0.70284E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.73           54509           26778           27272
v  Velocity[x]              0.293          2.0252         0.90807         0.90985
v  Velocity[y]           -0.38252         0.69319      0.00057324      0.00035278
v  Velocity[z]           -0.42236         0.51172      -0.0012586      -0.0013806
v  TurbEner             0.0010297        0.015898       0.0032865       0.0033456
v  Dissip              9.2136e-05        0.030933      0.00045067      0.00038968
v  TurbVisc               0.16863           11.34           4.716           5.277
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              150:        0.95700E-01

===============================================================


 INSTANT    0.151000000E+03   TIME STEP NUMBER             151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999876E+04
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 :  0.23769E+00 0.12383E+01
   Friction velocity        uet   :  0.14226E-01 0.72475E-01
   Friction velocity        uk    :  0.17576E-01 0.38774E-01
   Dimensionless distance   yplus :  0.43176E+03 0.95552E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63382E+01      53   0.12327E-02   0.20788E-01 
c  VelocityX    0.46304E+04      12   0.68167E-02   0.40034E-03 
c  VelocityY    0.46304E+04      12   0.68167E-02   0.28321E-04 
c  VelocityZ    0.46304E+04      12   0.68167E-02   0.49846E-04 
c  TurbEner     0.59771E+01      13   0.12797E-03   0.18659E-08 
c  Dissip       0.14263E+01      16   0.15444E-02   0.36809E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.26           54510           26778           27272
v  Velocity[x]            0.29269          2.1013         0.90807         0.90984
v  Velocity[y]           -0.36658         0.69954      0.00056118      0.00033733
v  Velocity[z]            -0.4222         0.50597      -0.0012727      -0.0013945
v  TurbEner             0.0010353        0.015274       0.0032867       0.0033457
v  Dissip              9.2173e-05        0.029882      0.00045069      0.00038969
v  TurbVisc               0.16869          11.379           4.716          5.2771
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              151:        0.95461E-01

===============================================================


 INSTANT    0.152000000E+03   TIME STEP NUMBER             152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000712E+04
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 :  0.23793E+00 0.13251E+01
   Friction velocity        uet   :  0.14241E-01 0.78993E-01
   Friction velocity        uk    :  0.17624E-01 0.38789E-01
   Dimensionless distance   yplus :  0.43211E+03 0.95504E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58943E+01      56   0.12370E-02   0.19319E-01 
c  VelocityX    0.46304E+04      12   0.69747E-02   0.39255E-03 
c  VelocityY    0.46304E+04      12   0.69747E-02   0.25512E-04 
c  VelocityZ    0.46304E+04      12   0.69747E-02   0.35319E-04 
c  TurbEner     0.59777E+01      12   0.63228E-04   0.60388E-09 
c  Dissip       0.14420E+01      14   0.33525E-03   0.33258E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.46           54513           26778           27273
v  Velocity[x]             0.2928          2.1571         0.90808         0.90986
v  Velocity[y]           -0.38225          0.6932      0.00055679      0.00033764
v  Velocity[z]           -0.41945         0.51112      -0.0012571      -0.0013778
v  TurbEner             0.0010389        0.015148       0.0032868       0.0033458
v  Dissip               9.218e-05        0.029879      0.00045092      0.00038984
v  TurbVisc               0.16903           11.37          4.7162          5.2772
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              152:        0.95421E-01

===============================================================


 INSTANT    0.153000000E+03   TIME STEP NUMBER             153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998568E+04
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 :  0.23726E+00 0.12145E+01
   Friction velocity        uet   :  0.14201E-01 0.72294E-01
   Friction velocity        uk    :  0.17654E-01 0.38835E-01
   Dimensionless distance   yplus :  0.43326E+03 0.95513E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63840E+01      55   0.15848E-02   0.20944E-01 
c  VelocityX    0.46304E+04      13   0.75300E-02   0.35250E-03 
c  VelocityY    0.46304E+04      13   0.75300E-02   0.25363E-04 
c  VelocityZ    0.46304E+04      13   0.75300E-02   0.38866E-04 
c  TurbEner     0.59787E+01      13   0.83642E-04   0.11315E-08 
c  Dissip       0.14686E+01      16   0.99484E-03   0.22984E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.95           54513           26778           27273
v  Velocity[x]            0.29275          2.1805         0.90808         0.90985
v  Velocity[y]             -0.367           0.702      0.00056452      0.00034321
v  Velocity[z]           -0.42042         0.50472      -0.0012663      -0.0013836
v  TurbEner             0.0010393        0.015264       0.0032871       0.0033461
v  Dissip              9.2177e-05        0.030352      0.00045127      0.00039007
v  TurbVisc               0.16975          11.308          4.7162          5.2773
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              153:        0.96032E-01

===============================================================


 INSTANT    0.154000000E+03   TIME STEP NUMBER             154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999876E+04
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 :  0.23780E+00 0.13246E+01
   Friction velocity        uet   :  0.14234E-01 0.78964E-01
   Friction velocity        uk    :  0.17658E-01 0.38881E-01
   Dimensionless distance   yplus :  0.43369E+03 0.95456E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64086E+01      56   0.13297E-02   0.21014E-01 
c  VelocityX    0.46304E+04      12   0.71207E-02   0.45020E-03 
c  VelocityY    0.46304E+04      12   0.71207E-02   0.41781E-04 
c  VelocityZ    0.46304E+04      12   0.71207E-02   0.13258E-03 
c  TurbEner     0.59788E+01      13   0.12374E-03   0.16315E-08 
c  Dissip       0.14867E+01      16   0.21078E-02   0.50888E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -167           54514           26779           27273
v  Velocity[x]             0.2929          2.0187         0.90806         0.90984
v  Velocity[y]           -0.38241           0.692      0.00056757      0.00034728
v  Velocity[z]           -0.42214         0.51171      -0.0012601      -0.0013805
v  TurbEner             0.0010435        0.015873       0.0032874       0.0033462
v  Dissip              9.2188e-05        0.032052       0.0004516       0.0003903
v  TurbVisc               0.16992          11.313          4.7163          5.2774
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              154:        0.95791E-01

===============================================================


 INSTANT    0.155000000E+03   TIME STEP NUMBER             155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998271E+04
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 :  0.23794E+00 0.12470E+01
   Friction velocity        uet   :  0.14242E-01 0.72722E-01
   Friction velocity        uk    :  0.17693E-01 0.38897E-01
   Dimensionless distance   yplus :  0.43366E+03 0.95491E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56749E+01      57   0.11922E-02   0.18606E-01 
c  VelocityX    0.46303E+04      12   0.63983E-02   0.34005E-03 
c  VelocityY    0.46303E+04      12   0.63983E-02   0.30289E-04 
c  VelocityZ    0.46303E+04      12   0.63983E-02   0.45066E-04 
c  TurbEner     0.59777E+01      13   0.14110E-03   0.19263E-08 
c  Dissip       0.14605E+01      16   0.18839E-02   0.50964E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.71           54522           26778           27272
v  Velocity[x]             0.2931          2.0954         0.90805         0.90983
v  Velocity[y]           -0.36684         0.70044      0.00055867      0.00033734
v  Velocity[z]           -0.42187         0.50573      -0.0012677      -0.0013857
v  TurbEner             0.0010477        0.015207       0.0032873       0.0033462
v  Dissip              9.2146e-05        0.030746      0.00045153      0.00039025
v  TurbVisc               0.16994          11.327          4.7164          5.2775
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              155:        0.95562E-01

===============================================================


 INSTANT    0.156000000E+03   TIME STEP NUMBER             156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001113E+04
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 :  0.23754E+00 0.13245E+01
   Friction velocity        uet   :  0.14218E-01 0.78955E-01
   Friction velocity        uk    :  0.17729E-01 0.38876E-01
   Dimensionless distance   yplus :  0.43505E+03 0.95543E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56835E+01      53   0.11802E-02   0.18645E-01 
c  VelocityX    0.46304E+04      12   0.63946E-02   0.32059E-03 
c  VelocityY    0.46304E+04      12   0.63946E-02   0.20841E-04 
c  VelocityZ    0.46304E+04      12   0.63946E-02   0.30121E-04 
c  TurbEner     0.59779E+01      12   0.66037E-04   0.55939E-09 
c  Dissip       0.14695E+01      13   0.34366E-03   0.23772E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.27           54538           26778           27273
v  Velocity[x]            0.29253          2.1498         0.90806         0.90984
v  Velocity[y]           -0.38288         0.69326      0.00055424      0.00033596
v  Velocity[z]            -0.4217         0.51048      -0.0012659      -0.0013843
v  TurbEner             0.0010457        0.015058       0.0032873       0.0033462
v  Dissip              9.2116e-05        0.030604      0.00045163      0.00039032
v  TurbVisc               0.17065          11.376          4.7164          5.2775
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              156:        0.94646E-01

===============================================================


 INSTANT    0.157000000E+03   TIME STEP NUMBER             157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000298E+04
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 :  0.23791E+00 0.12167E+01
   Friction velocity        uet   :  0.14240E-01 0.72532E-01
   Friction velocity        uk    :  0.17712E-01 0.38778E-01
   Dimensionless distance   yplus :  0.43499E+03 0.95530E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55881E+01      52   0.11848E-02   0.18319E-01 
c  VelocityX    0.46304E+04      12   0.72039E-02   0.30145E-03 
c  VelocityY    0.46304E+04      12   0.72039E-02   0.21101E-04 
c  VelocityZ    0.46304E+04      12   0.72039E-02   0.37117E-04 
c  TurbEner     0.59787E+01      13   0.64660E-04   0.84757E-09 
c  Dissip       0.14915E+01      15   0.82409E-03   0.15891E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.06           54549           26778           27272
v  Velocity[x]            0.29273          2.1742         0.90807         0.90984
v  Velocity[y]            -0.3674         0.70228      0.00055374        0.000332
v  Velocity[z]           -0.42177         0.50437      -0.0012743      -0.0013914
v  TurbEner             0.0010497        0.015148       0.0032874       0.0033463
v  Dissip              9.2096e-05        0.030944      0.00045187      0.00039048
v  TurbVisc               0.17041          11.358          4.7164          5.2775
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              157:        0.95416E-01

===============================================================


 INSTANT    0.158000000E+03   TIME STEP NUMBER             158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000670E+04
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 :  0.23778E+00 0.13237E+01
   Friction velocity        uet   :  0.14233E-01 0.78904E-01
   Friction velocity        uk    :  0.17746E-01 0.38802E-01
   Dimensionless distance   yplus :  0.43512E+03 0.95546E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75059E+01      58   0.15935E-02   0.24605E-01 
c  VelocityX    0.46303E+04      12   0.77576E-02   0.42549E-03 
c  VelocityY    0.46303E+04      12   0.77576E-02   0.48169E-04 
c  VelocityZ    0.46303E+04      12   0.77576E-02   0.13208E-03 
c  TurbEner     0.59794E+01      13   0.11652E-03   0.11662E-08 
c  Dissip       0.15081E+01      16   0.18520E-02   0.38112E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.34           54540           26778           27272
v  Velocity[x]            0.29265          2.0212         0.90806         0.90984
v  Velocity[y]           -0.38226         0.69525      0.00057064      0.00035032
v  Velocity[z]           -0.41943         0.51192      -0.0012594      -0.0013807
v  TurbEner             0.0010509         0.01572       0.0032877       0.0033466
v  Dissip              9.2099e-05        0.032429      0.00045219      0.00039073
v  TurbVisc               0.17039          11.361          4.7163          5.2775
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              158:        0.96200E-01

===============================================================


 INSTANT    0.159000000E+03   TIME STEP NUMBER             159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999402E+04
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 :  0.23728E+00 0.12171E+01
   Friction velocity        uet   :  0.14203E-01 0.72560E-01
   Friction velocity        uk    :  0.17756E-01 0.38847E-01
   Dimensionless distance   yplus :  0.43588E+03 0.95526E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.78136E+01      70   0.17098E-02   0.25640E-01 
c  VelocityX    0.46302E+04      12   0.68162E-02   0.43190E-03 
c  VelocityY    0.46302E+04      12   0.68162E-02   0.70353E-04 
c  VelocityZ    0.46302E+04      12   0.68162E-02   0.66520E-04 
c  TurbEner     0.59786E+01      14   0.13461E-03   0.23395E-08 
c  Dissip       0.14711E+01      16   0.21510E-02   0.65112E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.67           54518           26778           27273
v  Velocity[x]            0.29283          2.0866         0.90808         0.90985
v  Velocity[y]           -0.36606         0.70208      0.00055737      0.00033606
v  Velocity[z]            -0.4213         0.50658       -0.001268      -0.0013848
v  TurbEner             0.0010483         0.01513       0.0032877       0.0033466
v  Dissip              9.2085e-05        0.030952      0.00045202      0.00039062
v  TurbVisc               0.17067          11.332          4.7163          5.2775
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              159:        0.98608E-01

===============================================================


 INSTANT    0.160000000E+03   TIME STEP NUMBER             160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999576E+04
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 :  0.23774E+00 0.13254E+01
   Friction velocity        uet   :  0.14231E-01 0.78997E-01
   Friction velocity        uk    :  0.17734E-01 0.38865E-01
   Dimensionless distance   yplus :  0.43578E+03 0.95456E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64311E+01      59   0.13181E-02   0.21080E-01 
c  VelocityX    0.46303E+04      12   0.69940E-02   0.42597E-03 
c  VelocityY    0.46303E+04      12   0.69940E-02   0.35919E-04 
c  VelocityZ    0.46303E+04      12   0.69940E-02   0.29545E-04 
c  TurbEner     0.59788E+01      13   0.65316E-04   0.94174E-09 
c  Dissip       0.14757E+01      13   0.45779E-03   0.31538E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.7           54525           26778           27272
v  Velocity[x]            0.29286          2.1506         0.90806         0.90983
v  Velocity[y]            -0.3823         0.69551      0.00056493      0.00034722
v  Velocity[z]           -0.42255         0.51113      -0.0012662      -0.0013879
v  TurbEner             0.0010494        0.015013       0.0032878       0.0033467
v  Dissip              9.2104e-05         0.03066      0.00045202      0.00039062
v  TurbVisc               0.17038           11.33          4.7163          5.2774
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              160:        0.95940E-01

===============================================================


 INSTANT    0.161000000E+03   TIME STEP NUMBER             161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000595E+04
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 :  0.23786E+00 0.12138E+01
   Friction velocity        uet   :  0.14238E-01 0.72353E-01
   Friction velocity        uk    :  0.17743E-01 0.38816E-01
   Dimensionless distance   yplus :  0.43515E+03 0.95414E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60912E+01      55   0.11828E-02   0.19968E-01 
c  VelocityX    0.46303E+04      12   0.67682E-02   0.38099E-03 
c  VelocityY    0.46303E+04      12   0.67682E-02   0.26493E-04 
c  VelocityZ    0.46303E+04      12   0.67682E-02   0.46046E-04 
c  TurbEner     0.59796E+01      13   0.80557E-04   0.10303E-08 
c  Dissip       0.14959E+01      15   0.77981E-03   0.14006E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.76           54534           26777           27271
v  Velocity[x]            0.29285          2.1721         0.90806         0.90984
v  Velocity[y]           -0.36772         0.70327       0.0005631       0.0003395
v  Velocity[z]           -0.42144         0.50419      -0.0012744      -0.0013899
v  TurbEner              0.001051        0.015169       0.0032879       0.0033468
v  Dissip              9.2113e-05        0.030993      0.00045219      0.00039073
v  TurbVisc               0.16995           11.36          4.7163          5.2774
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              161:        0.95734E-01

===============================================================


 INSTANT    0.162000000E+03   TIME STEP NUMBER             162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001726E+04
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 :  0.23775E+00 0.13259E+01
   Friction velocity        uet   :  0.14231E-01 0.79035E-01
   Friction velocity        uk    :  0.17757E-01 0.38792E-01
   Dimensionless distance   yplus :  0.43603E+03 0.95351E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59464E+01      54   0.12985E-02   0.19498E-01 
c  VelocityX    0.46301E+04      12   0.65781E-02   0.33354E-03 
c  VelocityY    0.46301E+04      12   0.65781E-02   0.34195E-04 
c  VelocityZ    0.46301E+04      12   0.65781E-02   0.12030E-03 
c  TurbEner     0.59803E+01      12   0.12124E-03   0.11649E-08 
c  Dissip       0.15086E+01      16   0.19740E-02   0.43204E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.72           54541           26777           27271
v  Velocity[x]            0.29266          2.0116         0.90805         0.90984
v  Velocity[y]            -0.3824         0.69253      0.00056355      0.00034127
v  Velocity[z]           -0.42131         0.51167      -0.0012683      -0.0013892
v  TurbEner             0.0010462        0.015771       0.0032881        0.003347
v  Dissip               9.213e-05        0.032574      0.00045241      0.00039091
v  TurbVisc               0.17032          11.344          4.7163          5.2774
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              162:        0.95404E-01

===============================================================


 INSTANT    0.163000000E+03   TIME STEP NUMBER             163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001151E+04
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 :  0.23781E+00 0.12175E+01
   Friction velocity        uet   :  0.14235E-01 0.72572E-01
   Friction velocity        uk    :  0.17716E-01 0.38697E-01
   Dimensionless distance   yplus :  0.43538E+03 0.95344E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.51665E+01      53   0.10699E-02   0.16944E-01 
c  VelocityX    0.46302E+04      12   0.65181E-02   0.29957E-03 
c  VelocityY    0.46302E+04      12   0.65181E-02   0.24433E-04 
c  VelocityZ    0.46302E+04      12   0.65181E-02   0.45018E-04 
c  TurbEner     0.59791E+01      13   0.13789E-03   0.18857E-08 
c  Dissip       0.14795E+01      16   0.20529E-02   0.58847E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.65           54550           26777           27271
v  Velocity[x]            0.29285          2.0902         0.90806         0.90983
v  Velocity[y]           -0.36657         0.69983       0.0005597      0.00033681
v  Velocity[z]           -0.42309         0.50605        -0.00127      -0.0013895
v  TurbEner             0.0010473        0.015105        0.003288       0.0033469
v  Dissip              9.2129e-05        0.031161      0.00045225      0.00039081
v  TurbVisc               0.16974          11.359          4.7162          5.2773
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              163:        0.95475E-01

===============================================================


 INSTANT    0.164000000E+03   TIME STEP NUMBER             164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001037E+04
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 :  0.23749E+00 0.13238E+01
   Friction velocity        uet   :  0.14216E-01 0.78910E-01
   Friction velocity        uk    :  0.17725E-01 0.38748E-01
   Dimensionless distance   yplus :  0.43484E+03 0.95377E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60148E+01      54   0.15120E-02   0.19712E-01 
c  VelocityX    0.46302E+04      12   0.75643E-02   0.33445E-03 
c  VelocityY    0.46302E+04      12   0.75643E-02   0.22641E-04 
c  VelocityZ    0.46302E+04      12   0.75643E-02   0.32679E-04 
c  TurbEner     0.59795E+01      12   0.61226E-04   0.62268E-09 
c  Dissip       0.14858E+01      13   0.36971E-03   0.24289E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.33           54543           26777           27272
v  Velocity[x]            0.29296          2.1444         0.90807         0.90985
v  Velocity[y]           -0.38231         0.69512      0.00055655      0.00033758
v  Velocity[z]           -0.41908         0.51105      -0.0012575      -0.0013783
v  TurbEner             0.0010454        0.014946        0.003288        0.003347
v  Dissip              9.2076e-05        0.030965       0.0004523      0.00039086
v  TurbVisc               0.16937          11.339           4.716          5.2772
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              164:        0.95232E-01

===============================================================


 INSTANT    0.165000000E+03   TIME STEP NUMBER             165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998709E+04
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 :  0.23738E+00 0.12124E+01
   Friction velocity        uet   :  0.14208E-01 0.72269E-01
   Friction velocity        uk    :  0.17710E-01 0.38803E-01
   Dimensionless distance   yplus :  0.43489E+03 0.95359E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62045E+01      58   0.16869E-02   0.20353E-01 
c  VelocityX    0.46301E+04      13   0.71033E-02   0.42696E-03 
c  VelocityY    0.46301E+04      13   0.71033E-02   0.27271E-04 
c  VelocityZ    0.46301E+04      13   0.71033E-02   0.51835E-04 
c  TurbEner     0.59797E+01      13   0.94753E-04   0.12513E-08 
c  Dissip       0.14927E+01      15   0.14815E-02   0.27215E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.22           54518           26777           27272
v  Velocity[x]            0.29261          1.9934         0.90807         0.90984
v  Velocity[y]           -0.36701         0.70444      0.00056032      0.00034119
v  Velocity[z]           -0.42072         0.50474       -0.001269       -0.001387
v  TurbEner             0.0010406        0.015318       0.0032881       0.0033471
v  Dissip               9.208e-05        0.032071      0.00045246      0.00039099
v  TurbVisc                0.1693          11.335          4.7159           5.277
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              165:        0.96549E-01

===============================================================


 INSTANT    0.166000000E+03   TIME STEP NUMBER             166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999512E+04
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 :  0.23761E+00 0.13251E+01
   Friction velocity        uet   :  0.14222E-01 0.78984E-01
   Friction velocity        uk    :  0.17669E-01 0.38788E-01
   Dimensionless distance   yplus :  0.43435E+03 0.95389E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65772E+01      56   0.14812E-02   0.21569E-01 
c  VelocityX    0.46301E+04      12   0.63382E-02   0.37055E-03 
c  VelocityY    0.46301E+04      12   0.63382E-02   0.46883E-04 
c  VelocityZ    0.46301E+04      12   0.63382E-02   0.12005E-03 
c  TurbEner     0.59776E+01      14   0.14731E-03   0.24755E-08 
c  Dissip       0.14540E+01      17   0.25537E-02   0.88771E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.67           54526           26777           27272
v  Velocity[x]            0.29267          2.0775         0.90804         0.90981
v  Velocity[y]           -0.38248         0.69169      0.00057069      0.00034913
v  Velocity[z]           -0.42151         0.51177      -0.0012555      -0.0013783
v  TurbEner             0.0010393        0.014656        0.003288        0.003347
v  Dissip              9.2071e-05        0.030399      0.00045217      0.00039079
v  TurbVisc               0.16881          11.366          4.7157          5.2769
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              166:        0.96090E-01

===============================================================


 INSTANT    0.167000000E+03   TIME STEP NUMBER             167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000317E+04
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 :  0.23805E+00 0.12184E+01
   Friction velocity        uet   :  0.14247E-01 0.72621E-01
   Friction velocity        uk    :  0.17657E-01 0.38694E-01
   Dimensionless distance   yplus :  0.43330E+03 0.95409E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68924E+01      58   0.13937E-02   0.22607E-01 
c  VelocityX    0.46301E+04      12   0.62313E-02   0.30768E-03 
c  VelocityY    0.46301E+04      12   0.62313E-02   0.63246E-04 
c  VelocityZ    0.46301E+04      12   0.62313E-02   0.54741E-04 
c  TurbEner     0.59772E+01      13   0.67692E-04   0.95217E-09 
c  Dissip       0.14473E+01      14   0.78665E-03   0.80586E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.29           54536           26777           27271
v  Velocity[x]            0.29308           2.123         0.90805         0.90982
v  Velocity[y]           -0.36691         0.70055      0.00055801      0.00033368
v  Velocity[z]           -0.42105         0.50569       -0.001267      -0.0013832
v  TurbEner             0.0010387        0.014555       0.0032878       0.0033469
v  Dissip              9.2053e-05        0.029899      0.00045205      0.00039071
v  TurbVisc               0.16821          11.343          4.7156          5.2767
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              167:        0.95795E-01

===============================================================


 INSTANT    0.168000000E+03   TIME STEP NUMBER             168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000252E+04
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 :  0.23778E+00 0.13238E+01
   Friction velocity        uet   :  0.14230E-01 0.78902E-01
   Friction velocity        uk    :  0.17652E-01 0.38714E-01
   Dimensionless distance   yplus :  0.43379E+03 0.95401E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62825E+01      56   0.11915E-02   0.20597E-01 
c  VelocityX    0.46301E+04      12   0.74862E-02   0.33338E-03 
c  VelocityY    0.46301E+04      12   0.74862E-02   0.38897E-04 
c  VelocityZ    0.46301E+04      12   0.74862E-02   0.30697E-04 
c  TurbEner     0.59783E+01      12   0.64663E-04   0.65915E-09 
c  Dissip       0.14605E+01      14   0.50080E-03   0.60786E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.22           54543           26778           27272
v  Velocity[x]            0.29245          2.1718         0.90805         0.90983
v  Velocity[y]           -0.38284           0.694      0.00056004        0.000339
v  Velocity[z]           -0.42268         0.51053      -0.0012604      -0.0013808
v  TurbEner             0.0010319        0.014637       0.0032877       0.0033468
v  Dissip              9.2072e-05         0.02996      0.00045208      0.00039074
v  TurbVisc               0.16844          11.346          4.7154          5.2765
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              168:        0.95614E-01

===============================================================


 INSTANT    0.169000000E+03   TIME STEP NUMBER             169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998465E+04
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 :  0.23763E+00 0.12166E+01
   Friction velocity        uet   :  0.14220E-01 0.72526E-01
   Friction velocity        uk    :  0.17595E-01 0.38701E-01
   Dimensionless distance   yplus :  0.43275E+03 0.95439E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62986E+01      65   0.13801E-02   0.20646E-01 
c  VelocityX    0.46300E+04      12   0.67630E-02   0.41143E-03 
c  VelocityY    0.46300E+04      12   0.67630E-02   0.33749E-04 
c  VelocityZ    0.46300E+04      12   0.67630E-02   0.43457E-04 
c  TurbEner     0.59785E+01      13   0.11686E-03   0.12197E-08 
c  Dissip       0.14675E+01      16   0.17416E-02   0.31095E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.79           54551           26776           27271
v  Velocity[x]            0.29278          2.0023         0.90806         0.90983
v  Velocity[y]           -0.36734         0.70274      0.00055736      0.00033401
v  Velocity[z]           -0.42168         0.50436      -0.0012755      -0.0013927
v  TurbEner              0.001032        0.015206       0.0032877       0.0033469
v  Dissip              9.2069e-05        0.031309      0.00045219      0.00039083
v  TurbVisc               0.16776           11.32          4.7152          5.2764
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              169:        0.97486E-01

===============================================================


 INSTANT    0.170000000E+03   TIME STEP NUMBER             170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001651E+04
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 :  0.23788E+00 0.13234E+01
   Friction velocity        uet   :  0.14234E-01 0.78880E-01
   Friction velocity        uk    :  0.17596E-01 0.38765E-01
   Dimensionless distance   yplus :  0.43198E+03 0.95400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64209E+01      67   0.15625E-02   0.21033E-01 
c  VelocityX    0.46300E+04      12   0.70041E-02   0.34997E-03 
c  VelocityY    0.46300E+04      12   0.70041E-02   0.36829E-04 
c  VelocityZ    0.46300E+04      12   0.70041E-02   0.10618E-03 
c  TurbEner     0.59779E+01      13   0.12362E-03   0.17766E-08 
c  Dissip       0.14358E+01      17   0.22128E-02   0.71608E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.19           54540           26776           27271
v  Velocity[x]            0.29295          2.0862         0.90806         0.90984
v  Velocity[y]            -0.3822         0.69554      0.00056503       0.0003443
v  Velocity[z]            -0.4201         0.51184      -0.0012531      -0.0013748
v  TurbEner             0.0010303        0.014672       0.0032876       0.0033468
v  Dissip               9.209e-05        0.029931      0.00045193      0.00039066
v  TurbVisc                0.1674          11.312           4.715          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              170:        0.96779E-01

===============================================================


 INSTANT    0.171000000E+03   TIME STEP NUMBER             171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000147E+04
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 :  0.23714E+00 0.12171E+01
   Friction velocity        uet   :  0.14189E-01 0.72553E-01
   Friction velocity        uk    :  0.17581E-01 0.38784E-01
   Dimensionless distance   yplus :  0.43207E+03 0.95367E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63798E+01      66   0.15510E-02   0.20940E-01 
c  VelocityX    0.46301E+04      12   0.61329E-02   0.40017E-03 
c  VelocityY    0.46301E+04      12   0.61329E-02   0.34254E-04 
c  VelocityZ    0.46301E+04      12   0.61329E-02   0.54704E-04 
c  TurbEner     0.59780E+01      13   0.74193E-04   0.99753E-09 
c  Dissip       0.14344E+01      14   0.60857E-03   0.54475E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.06           54517           26777           27271
v  Velocity[x]            0.29252          2.1384         0.90807         0.90984
v  Velocity[y]           -0.36603         0.70109      0.00056188      0.00034249
v  Velocity[z]           -0.41985         0.50662      -0.0012618      -0.0013806
v  TurbEner             0.0010258        0.014583       0.0032876       0.0033468
v  Dissip              9.2031e-05        0.029567      0.00045189      0.00039065
v  TurbVisc               0.16748           11.34          4.7149           5.276
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              171:        0.97907E-01

===============================================================


 INSTANT    0.172000000E+03   TIME STEP NUMBER             172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999300E+04
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 :  0.23794E+00 0.13257E+01
   Friction velocity        uet   :  0.14235E-01 0.79015E-01
   Friction velocity        uk    :  0.17543E-01 0.38784E-01
   Dimensionless distance   yplus :  0.43149E+03 0.95385E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57822E+01      52   0.11875E-02   0.18949E-01 
c  VelocityX    0.46301E+04      12   0.70934E-02   0.33828E-03 
c  VelocityY    0.46301E+04      12   0.70934E-02   0.24894E-04 
c  VelocityZ    0.46301E+04      12   0.70934E-02   0.32277E-04 
c  TurbEner     0.59782E+01      13   0.70492E-04   0.10449E-08 
c  Dissip       0.14523E+01      15   0.69122E-03   0.11092E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.95           54525           26777           27271
v  Velocity[x]            0.29256          2.1773         0.90806         0.90983
v  Velocity[y]           -0.38232          0.6946      0.00055834      0.00033998
v  Velocity[z]           -0.42167         0.51109      -0.0012527      -0.0013732
v  TurbEner             0.0010255        0.014706       0.0032876       0.0033468
v  Dissip              9.2062e-05        0.029805      0.00045199      0.00039072
v  TurbVisc               0.16709           11.39          4.7147          5.2759
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              172:        0.94915E-01

===============================================================


 INSTANT    0.173000000E+03   TIME STEP NUMBER             173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999762E+04
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 :  0.23790E+00 0.12137E+01
   Friction velocity        uet   :  0.14232E-01 0.72308E-01
   Friction velocity        uk    :  0.17540E-01 0.38772E-01
   Dimensionless distance   yplus :  0.43050E+03 0.95349E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65829E+01      57   0.14595E-02   0.21578E-01 
c  VelocityX    0.46300E+04      12   0.66428E-02   0.37280E-03 
c  VelocityY    0.46300E+04      12   0.66428E-02   0.40444E-04 
c  VelocityZ    0.46300E+04      12   0.66428E-02   0.40550E-04 
c  TurbEner     0.59786E+01      13   0.12348E-03   0.13810E-08 
c  Dissip       0.14632E+01      16   0.18739E-02   0.37463E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.79           54533           26776           27270
v  Velocity[x]            0.29329          2.0061         0.90805         0.90982
v  Velocity[y]           -0.36769         0.70283      0.00055112      0.00033168
v  Velocity[z]           -0.42269         0.50421      -0.0012719      -0.0013911
v  TurbEner             0.0010261        0.015291       0.0032877       0.0033469
v  Dissip              9.2063e-05        0.031258      0.00045212      0.00039081
v  TurbVisc               0.16662          11.373          4.7146          5.2757
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              173:        0.95579E-01

===============================================================


 INSTANT    0.174000000E+03   TIME STEP NUMBER             174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002222E+04
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 :  0.23748E+00 0.13252E+01
   Friction velocity        uet   :  0.14206E-01 0.78991E-01
   Friction velocity        uk    :  0.17545E-01 0.38787E-01
   Dimensionless distance   yplus :  0.43116E+03 0.95334E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67131E+01      65   0.14318E-02   0.22015E-01 
c  VelocityX    0.46300E+04      12   0.68359E-02   0.34526E-03 
c  VelocityY    0.46300E+04      12   0.68359E-02   0.50832E-04 
c  VelocityZ    0.46300E+04      12   0.68359E-02   0.11810E-03 
c  TurbEner     0.59778E+01      13   0.12218E-03   0.17751E-08 
c  Dissip       0.14366E+01      16   0.20299E-02   0.60997E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.97           54542           26776           27270
v  Velocity[x]            0.29285          2.0913         0.90804         0.90982
v  Velocity[y]            -0.3825         0.69251      0.00056066      0.00034176
v  Velocity[z]           -0.42118         0.51172      -0.0012557      -0.0013782
v  TurbEner             0.0010208         0.01477       0.0032874       0.0033467
v  Dissip              9.2056e-05        0.029984      0.00045189      0.00039065
v  TurbVisc               0.16699          11.374          4.7145          5.2756
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              174:        0.96806E-01

===============================================================


 INSTANT    0.175000000E+03   TIME STEP NUMBER             175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999978E+04
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 :  0.23815E+00 0.12174E+01
   Friction velocity        uet   :  0.14245E-01 0.72562E-01
   Friction velocity        uk    :  0.17500E-01 0.38729E-01
   Dimensionless distance   yplus :  0.43037E+03 0.95363E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63101E+01      54   0.12946E-02   0.20688E-01 
c  VelocityX    0.46300E+04      12   0.64240E-02   0.38812E-03 
c  VelocityY    0.46300E+04      12   0.64240E-02   0.32221E-04 
c  VelocityZ    0.46300E+04      12   0.64240E-02   0.54615E-04 
c  TurbEner     0.59779E+01      12   0.66914E-04   0.72048E-09 
c  Dissip       0.14369E+01      14   0.53704E-03   0.42325E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.57           54550           26776           27271
v  Velocity[x]            0.29263          2.1392         0.90807         0.90984
v  Velocity[y]           -0.36652         0.70004      0.00056163      0.00033939
v  Velocity[z]           -0.42257         0.50597      -0.0012774      -0.0013963
v  TurbEner             0.0010223        0.014695       0.0032874       0.0033467
v  Dissip              9.2099e-05        0.029678      0.00045187      0.00039064
v  TurbVisc               0.16646          11.346          4.7143          5.2755
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              175:        0.95756E-01

===============================================================


 INSTANT    0.176000000E+03   TIME STEP NUMBER             176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998870E+04
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 :  0.23774E+00 0.13240E+01
   Friction velocity        uet   :  0.14220E-01 0.78916E-01
   Friction velocity        uk    :  0.17513E-01 0.38728E-01
   Dimensionless distance   yplus :  0.42985E+03 0.95340E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61536E+01      54   0.14063E-02   0.20167E-01 
c  VelocityX    0.46301E+04      12   0.76251E-02   0.37900E-03 
c  VelocityY    0.46301E+04      12   0.76251E-02   0.22324E-04 
c  VelocityZ    0.46301E+04      12   0.76251E-02   0.34894E-04 
c  TurbEner     0.59789E+01      13   0.84167E-04   0.94739E-09 
c  Dissip       0.14552E+01      15   0.71320E-03   0.11992E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.57           54540           26776           27270
v  Velocity[x]            0.29304          2.1804         0.90808         0.90986
v  Velocity[y]           -0.38224         0.69313      0.00055834      0.00034029
v  Velocity[z]            -0.4188         0.51104      -0.0012642      -0.0013831
v  TurbEner             0.0010218        0.014803       0.0032875       0.0033467
v  Dissip              9.2102e-05        0.029881      0.00045198       0.0003907
v  TurbVisc               0.16622          11.345          4.7142          5.2754
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              176:        0.95363E-01

===============================================================


 INSTANT    0.177000000E+03   TIME STEP NUMBER             177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999923E+04
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 :  0.23747E+00 0.12165E+01
   Friction velocity        uet   :  0.14204E-01 0.72522E-01
   Friction velocity        uk    :  0.17508E-01 0.38755E-01
   Dimensionless distance   yplus :  0.43014E+03 0.95334E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75900E+01      59   0.17705E-02   0.24891E-01 
c  VelocityX    0.46300E+04      13   0.74461E-02   0.48688E-03 
c  VelocityY    0.46300E+04      13   0.74461E-02   0.44229E-04 
c  VelocityZ    0.46300E+04      13   0.74461E-02   0.45951E-04 
c  TurbEner     0.59795E+01      13   0.11942E-03   0.17421E-08 
c  Dissip       0.14663E+01      16   0.18512E-02   0.37516E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.71           54516           26776           27271
v  Velocity[x]            0.29282          2.0066         0.90808         0.90985
v  Velocity[y]           -0.36694         0.70194      0.00056081      0.00034113
v  Velocity[z]           -0.42065         0.50473      -0.0012684      -0.0013843
v  TurbEner             0.0010189        0.015389       0.0032876       0.0033468
v  Dissip              9.2114e-05        0.031323      0.00045217      0.00039085
v  TurbVisc                0.1664           11.32          4.7141          5.2753
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              177:        0.96895E-01

===============================================================


 INSTANT    0.178000000E+03   TIME STEP NUMBER             178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999795E+04
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 :  0.23770E+00 0.13236E+01
   Friction velocity        uet   :  0.14217E-01 0.78898E-01
   Friction velocity        uk    :  0.17484E-01 0.38681E-01
   Dimensionless distance   yplus :  0.42989E+03 0.95330E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70027E+01      60   0.13406E-02   0.22959E-01 
c  VelocityX    0.46300E+04      12   0.67208E-02   0.45128E-03 
c  VelocityY    0.46300E+04      12   0.67208E-02   0.57362E-04 
c  VelocityZ    0.46300E+04      12   0.67208E-02   0.12292E-03 
c  TurbEner     0.59780E+01      14   0.13082E-03   0.25506E-08 
c  Dissip       0.14380E+01      16   0.20177E-02   0.61713E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.81           54522           26776           27271
v  Velocity[x]             0.2925           2.093         0.90805         0.90983
v  Velocity[y]           -0.38236         0.69463       0.0005687      0.00034893
v  Velocity[z]           -0.42209         0.51175       -0.001256      -0.0013755
v  TurbEner             0.0010201        0.014865       0.0032874       0.0033466
v  Dissip              9.2081e-05        0.030054      0.00045194      0.00039069
v  TurbVisc               0.16618          11.313           4.714          5.2751
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              178:        0.96496E-01

===============================================================


 INSTANT    0.179000000E+03   TIME STEP NUMBER             179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000814E+04
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 :  0.23781E+00 0.12166E+01
   Friction velocity        uet   :  0.14223E-01 0.72526E-01
   Friction velocity        uk    :  0.17493E-01 0.38755E-01
   Dimensionless distance   yplus :  0.42928E+03 0.95311E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59020E+01      57   0.13038E-02   0.19344E-01 
c  VelocityX    0.46299E+04      12   0.66667E-02   0.37253E-03 
c  VelocityY    0.46299E+04      12   0.66667E-02   0.32694E-04 
c  VelocityZ    0.46299E+04      12   0.66667E-02   0.54344E-04 
c  TurbEner     0.59779E+01      13   0.73852E-04   0.91578E-09 
c  Dissip       0.14418E+01      14   0.49200E-03   0.42801E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.82           54523           26776           27270
v  Velocity[x]            0.29304          2.1401         0.90805         0.90983
v  Velocity[y]           -0.36679         0.70179      0.00057017      0.00034661
v  Velocity[z]           -0.42102         0.50579      -0.0012669      -0.0013855
v  TurbEner             0.0010225        0.014801       0.0032873       0.0033465
v  Dissip              9.2072e-05        0.029811      0.00045191      0.00039066
v  TurbVisc               0.16588           11.34          4.7138           5.275
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              179:        0.95854E-01

===============================================================


 INSTANT    0.180000000E+03   TIME STEP NUMBER             180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001757E+04
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 :  0.23776E+00 0.13256E+01
   Friction velocity        uet   :  0.14220E-01 0.79011E-01
   Friction velocity        uk    :  0.17514E-01 0.38810E-01
   Dimensionless distance   yplus :  0.43026E+03 0.95313E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59949E+01      66   0.14539E-02   0.19667E-01 
c  VelocityX    0.46300E+04      13   0.69376E-02   0.33571E-03 
c  VelocityY    0.46300E+04      13   0.69376E-02   0.22191E-04 
c  VelocityZ    0.46300E+04      13   0.69376E-02   0.29578E-04 
c  TurbEner     0.59787E+01      12   0.68221E-04   0.79762E-09 
c  Dissip       0.14609E+01      15   0.76460E-03   0.13829E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.39           54511           26777           27272
v  Velocity[x]            0.29251          2.1801         0.90805         0.90984
v  Velocity[y]           -0.38285         0.69489      0.00056878      0.00035194
v  Velocity[z]           -0.42086         0.51051      -0.0012535      -0.0013745
v  TurbEner             0.0010188        0.014896       0.0032873       0.0033465
v  Dissip              9.2074e-05         0.03004      0.00045208      0.00039077
v  TurbVisc               0.16642           11.32          4.7137          5.2749
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              180:        0.98761E-01

===============================================================


 INSTANT    0.181000000E+03   TIME STEP NUMBER             181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998167E+04
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 :  0.23782E+00 0.12142E+01
   Friction velocity        uet   :  0.14223E-01 0.72349E-01
   Friction velocity        uk    :  0.17483E-01 0.38728E-01
   Dimensionless distance   yplus :  0.42980E+03 0.95244E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59679E+01      53   0.12876E-02   0.19570E-01 
c  VelocityX    0.46300E+04      13   0.66137E-02   0.36787E-03 
c  VelocityY    0.46300E+04      13   0.66137E-02   0.45004E-04 
c  VelocityZ    0.46300E+04      13   0.66137E-02   0.32004E-04 
c  TurbEner     0.59782E+01      13   0.11721E-03   0.16635E-08 
c  Dissip       0.14735E+01      16   0.18480E-02   0.37870E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.66           54517           26777           27271
v  Velocity[x]             0.2928          2.0103         0.90805         0.90982
v  Velocity[y]           -0.36742         0.70298      0.00057065       0.0003481
v  Velocity[z]           -0.42285         0.50435      -0.0012665      -0.0013892
v  TurbEner             0.0010218        0.015471       0.0032872       0.0033464
v  Dissip              9.2051e-05        0.031489      0.00045221      0.00039087
v  TurbVisc               0.16605          11.327          4.7136          5.2747
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              181:        0.96091E-01

===============================================================


 INSTANT    0.182000000E+03   TIME STEP NUMBER             182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000355E+04
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 :  0.23758E+00 0.13257E+01
   Friction velocity        uet   :  0.14209E-01 0.79022E-01
   Friction velocity        uk    :  0.17508E-01 0.38753E-01
   Dimensionless distance   yplus :  0.42959E+03 0.95230E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60375E+01      52   0.13070E-02   0.19801E-01 
c  VelocityX    0.46300E+04      12   0.67268E-02   0.30571E-03 
c  VelocityY    0.46300E+04      12   0.67268E-02   0.22274E-04 
c  VelocityZ    0.46300E+04      12   0.67268E-02   0.52713E-04 
c  TurbEner     0.59768E+01      13   0.12409E-03   0.17555E-08 
c  Dissip       0.14413E+01      16   0.20023E-02   0.62552E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.34           54532           26777           27271
v  Velocity[x]            0.29308          2.0902         0.90805         0.90983
v  Velocity[y]           -0.38224         0.69259       0.0005577      0.00033683
v  Velocity[z]           -0.41977         0.51192      -0.0012604      -0.0013824
v  TurbEner             0.0010227        0.014927       0.0032869       0.0033461
v  Dissip              9.1983e-05         0.03025      0.00045196      0.00039069
v  TurbVisc               0.16596          11.364          4.7134          5.2746
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              182:        0.95463E-01

===============================================================


 INSTANT    0.183000000E+03   TIME STEP NUMBER             183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000808E+04
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 :  0.23757E+00 0.12345E+01
   Friction velocity        uet   :  0.14208E-01 0.72562E-01
   Friction velocity        uk    :  0.17516E-01 0.38784E-01
   Dimensionless distance   yplus :  0.43018E+03 0.95221E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57222E+01      53   0.13269E-02   0.18760E-01 
c  VelocityX    0.46300E+04      12   0.62071E-02   0.26619E-03 
c  VelocityY    0.46300E+04      12   0.62071E-02   0.25511E-04 
c  VelocityZ    0.46300E+04      12   0.62071E-02   0.39276E-04 
c  TurbEner     0.59769E+01      12   0.67823E-04   0.63675E-09 
c  Dissip       0.14493E+01      13   0.42799E-03   0.28511E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.69           54543           26776           27271
v  Velocity[x]            0.29261          2.1416         0.90806         0.90983
v  Velocity[y]           -0.36607         0.70032      0.00055961      0.00033732
v  Velocity[z]            -0.4203         0.50651      -0.0012689      -0.0013895
v  TurbEner             0.0010207        0.014833       0.0032867       0.0033459
v  Dissip              9.1987e-05        0.030021       0.0004519      0.00039064
v  TurbVisc               0.16628          11.343          4.7132          5.2744
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              183:        0.95458E-01

===============================================================


 INSTANT    0.184000000E+03   TIME STEP NUMBER             184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000809E+04
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 :  0.23782E+00 0.13236E+01
   Friction velocity        uet   :  0.14223E-01 0.78893E-01
   Friction velocity        uk    :  0.17499E-01 0.38809E-01
   Dimensionless distance   yplus :  0.43011E+03 0.95241E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56866E+01      54   0.12587E-02   0.18646E-01 
c  VelocityX    0.46300E+04      12   0.72198E-02   0.26690E-03 
c  VelocityY    0.46300E+04      12   0.72198E-02   0.34801E-04 
c  VelocityZ    0.46300E+04      12   0.72198E-02   0.90822E-04 
c  TurbEner     0.59778E+01      12   0.66204E-04   0.66313E-09 
c  Dissip       0.14713E+01      15   0.80383E-03   0.15153E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.58           54550           26777           27271
v  Velocity[x]            0.29268          2.1848         0.90806         0.90983
v  Velocity[y]           -0.38227         0.69538      0.00056347      0.00034357
v  Velocity[z]           -0.42124         0.51114      -0.0012595       -0.001382
v  TurbEner             0.0010223        0.014933       0.0032867       0.0033459
v  Dissip              9.1983e-05        0.030302      0.00045201       0.0003907
v  TurbVisc               0.16614          11.345          4.7131          5.2743
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              184:        0.95056E-01

===============================================================


 INSTANT    0.185000000E+03   TIME STEP NUMBER             185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000780E+04
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 :  0.23811E+00 0.12129E+01
   Friction velocity        uet   :  0.14240E-01 0.72301E-01
   Friction velocity        uk    :  0.17512E-01 0.38793E-01
   Dimensionless distance   yplus :  0.42957E+03 0.95252E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60692E+01      55   0.15899E-02   0.19893E-01 
c  VelocityX    0.46299E+04      13   0.69617E-02   0.39502E-03 
c  VelocityY    0.46299E+04      13   0.69617E-02   0.26520E-04 
c  VelocityZ    0.46299E+04      13   0.69617E-02   0.37905E-04 
c  TurbEner     0.59784E+01      13   0.12080E-03   0.13210E-08 
c  Dissip       0.14910E+01      16   0.21565E-02   0.53802E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.22           54543           26776           27270
v  Velocity[x]            0.29307          2.0199         0.90805         0.90983
v  Velocity[y]           -0.36774         0.70418      0.00056987      0.00034842
v  Velocity[z]           -0.42167         0.50418      -0.0012614      -0.0013799
v  TurbEner             0.0010243        0.015543       0.0032867       0.0033459
v  Dissip              9.2018e-05        0.031985      0.00045222      0.00039085
v  TurbVisc                0.1659          11.321          4.7131          5.2742
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              185:        0.96008E-01

===============================================================


 INSTANT    0.186000000E+03   TIME STEP NUMBER             186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001642E+04
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 :  0.23767E+00 0.13246E+01
   Friction velocity        uet   :  0.14214E-01 0.78956E-01
   Friction velocity        uk    :  0.17530E-01 0.38766E-01
   Dimensionless distance   yplus :  0.43050E+03 0.95274E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62533E+01      56   0.16541E-02   0.20500E-01 
c  VelocityX    0.46299E+04      13   0.63785E-02   0.36244E-03 
c  VelocityY    0.46299E+04      13   0.63785E-02   0.27343E-04 
c  VelocityZ    0.46299E+04      13   0.63785E-02   0.53357E-04 
c  TurbEner     0.59775E+01      14   0.13599E-03   0.23731E-08 
c  Dissip       0.14617E+01      16   0.19923E-02   0.61328E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.08           54518           26777           27271
v  Velocity[x]            0.29268          2.0911         0.90806         0.90983
v  Velocity[y]           -0.38244          0.6919      0.00056929      0.00034824
v  Velocity[z]           -0.42237         0.51167      -0.0012542      -0.0013757
v  TurbEner              0.001021         0.01495       0.0032866       0.0033459
v  Dissip              9.2047e-05        0.030727      0.00045203      0.00039074
v  TurbVisc               0.16644          11.315           4.713          5.2742
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              186:        0.96333E-01

===============================================================


 INSTANT    0.187000000E+03   TIME STEP NUMBER             187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998509E+04
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 :  0.23767E+00 0.12180E+01
   Friction velocity        uet   :  0.14215E-01 0.72595E-01
   Friction velocity        uk    :  0.17502E-01 0.38674E-01
   Dimensionless distance   yplus :  0.43013E+03 0.95308E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57592E+01      56   0.12248E-02   0.18881E-01 
c  VelocityX    0.46300E+04      12   0.66008E-02   0.38382E-03 
c  VelocityY    0.46300E+04      12   0.66008E-02   0.28273E-04 
c  VelocityZ    0.46300E+04      12   0.66008E-02   0.37543E-04 
c  TurbEner     0.59769E+01      13   0.79929E-04   0.10181E-08 
c  Dissip       0.14649E+01      14   0.52912E-03   0.42352E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.17           54528           26777           27271
v  Velocity[x]            0.29278          2.1429         0.90804         0.90982
v  Velocity[y]           -0.36654         0.70117      0.00057206      0.00034852
v  Velocity[z]           -0.42225         0.50609       -0.001271      -0.0013876
v  TurbEner             0.0010243        0.014787       0.0032866       0.0033459
v  Dissip              9.2077e-05         0.03042      0.00045201      0.00039072
v  TurbVisc               0.16617          11.346           4.713          5.2742
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              187:        0.96520E-01

===============================================================


 INSTANT    0.188000000E+03   TIME STEP NUMBER             188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998098E+04
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 :  0.23795E+00 0.13237E+01
   Friction velocity        uet   :  0.14231E-01 0.78895E-01
   Friction velocity        uk    :  0.17529E-01 0.38705E-01
   Dimensionless distance   yplus :  0.43006E+03 0.95275E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64367E+01      63   0.13561E-02   0.21102E-01 
c  VelocityX    0.46299E+04      12   0.63562E-02   0.33130E-03 
c  VelocityY    0.46299E+04      12   0.63562E-02   0.35324E-04 
c  VelocityZ    0.46299E+04      12   0.63562E-02   0.31721E-04 
c  TurbEner     0.59776E+01      13   0.65147E-04   0.72547E-09 
c  Dissip       0.14879E+01      15   0.70372E-03   0.11934E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.77           54536           26778           27272
v  Velocity[x]             0.2927          2.1864         0.90803         0.90981
v  Velocity[y]            -0.3822          0.6952       0.0005661      0.00034305
v  Velocity[z]           -0.41963         0.51112      -0.0012539      -0.0013733
v  TurbEner             0.0010251         0.01485       0.0032866       0.0033459
v  Dissip              9.2139e-05         0.03062      0.00045215      0.00039081
v  TurbVisc                0.1662          11.393           4.713          5.2742
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              188:        0.96007E-01

===============================================================


 INSTANT    0.189000000E+03   TIME STEP NUMBER             189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997972E+04
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 :  0.23746E+00 0.12173E+01
   Friction velocity        uet   :  0.14203E-01 0.72566E-01
   Friction velocity        uk    :  0.17537E-01 0.38764E-01
   Dimensionless distance   yplus :  0.43073E+03 0.95270E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62405E+01      62   0.14548E-02   0.20471E-01 
c  VelocityX    0.46299E+04      13   0.69852E-02   0.35857E-03 
c  VelocityY    0.46299E+04      13   0.69852E-02   0.46798E-04 
c  VelocityZ    0.46299E+04      13   0.69852E-02   0.44939E-04 
c  TurbEner     0.59776E+01      13   0.11767E-03   0.15086E-08 
c  Dissip       0.14974E+01      16   0.18734E-02   0.40218E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.84           54544           26778           27272
v  Velocity[x]            0.29287          2.0132         0.90805         0.90983
v  Velocity[y]           -0.36696         0.70184      0.00055779      0.00033538
v  Velocity[z]            -0.4205         0.50478      -0.0012773      -0.0013948
v  TurbEner             0.0010224        0.015425       0.0032865       0.0033458
v  Dissip              9.2152e-05        0.032064      0.00045234      0.00039096
v  TurbVisc               0.16659          11.382           4.713          5.2742
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              189:        0.97343E-01

===============================================================


 INSTANT    0.190000000E+03   TIME STEP NUMBER             190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999896E+04
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 :  0.23785E+00 0.13267E+01
   Friction velocity        uet   :  0.14227E-01 0.79086E-01
   Friction velocity        uk    :  0.17514E-01 0.38787E-01
   Dimensionless distance   yplus :  0.43059E+03 0.95236E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67112E+01      64   0.13504E-02   0.21998E-01 
c  VelocityX    0.46299E+04      12   0.68149E-02   0.37777E-03 
c  VelocityY    0.46299E+04      12   0.68149E-02   0.38831E-04 
c  VelocityZ    0.46299E+04      12   0.68149E-02   0.12281E-03 
c  TurbEner     0.59767E+01      13   0.12321E-03   0.17213E-08 
c  Dissip       0.14671E+01      17   0.21533E-02   0.70962E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.49           54552           26777           27271
v  Velocity[x]            0.29286          2.0991         0.90803         0.90982
v  Velocity[y]            -0.3824         0.69524      0.00056452       0.0003442
v  Velocity[z]            -0.4211         0.51177      -0.0012576      -0.0013803
v  TurbEner             0.0010236        0.014901       0.0032862       0.0033456
v  Dissip               9.216e-05        0.030726       0.0004521       0.0003908
v  TurbVisc               0.16643          11.332          4.7128           5.274
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              190:        0.97740E-01

===============================================================


 INSTANT    0.191000000E+03   TIME STEP NUMBER             191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001203E+04
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 :  0.23801E+00 0.12147E+01
   Friction velocity        uet   :  0.14237E-01 0.72369E-01
   Friction velocity        uk    :  0.17524E-01 0.38768E-01
   Dimensionless distance   yplus :  0.42998E+03 0.95195E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67212E+01      56   0.16474E-02   0.22025E-01 
c  VelocityX    0.46299E+04      12   0.71959E-02   0.36551E-03 
c  VelocityY    0.46299E+04      12   0.71959E-02   0.45729E-04 
c  VelocityZ    0.46299E+04      12   0.71959E-02   0.54002E-04 
c  TurbEner     0.59768E+01      12   0.64068E-04   0.64043E-09 
c  Dissip       0.14686E+01      14   0.47286E-03   0.38288E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.95           54541           26776           27271
v  Velocity[x]            0.29306          2.1455         0.90807         0.90985
v  Velocity[y]           -0.36688         0.70417      0.00056395       0.0003419
v  Velocity[z]           -0.42214         0.50566      -0.0012579      -0.0013749
v  TurbEner             0.0010254        0.014853       0.0032861       0.0033455
v  Dissip              9.2113e-05         0.03048      0.00045206      0.00039077
v  TurbVisc               0.16616           11.32          4.7127          5.2739
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              191:        0.95144E-01

===============================================================


 INSTANT    0.192000000E+03   TIME STEP NUMBER             192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002105E+04
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 :  0.23737E+00 0.13245E+01
   Friction velocity        uet   :  0.14199E-01 0.78953E-01
   Friction velocity        uk    :  0.17539E-01 0.38746E-01
   Dimensionless distance   yplus :  0.43092E+03 0.95263E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65912E+01      56   0.15872E-02   0.21618E-01 
c  VelocityX    0.46300E+04      13   0.73889E-02   0.41984E-03 
c  VelocityY    0.46300E+04      13   0.73889E-02   0.28341E-04 
c  VelocityZ    0.46300E+04      13   0.73889E-02   0.37875E-04 
c  TurbEner     0.59780E+01      13   0.79423E-04   0.12501E-08 
c  Dissip       0.14916E+01      15   0.78709E-03   0.14493E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.38           54515           26777           27271
v  Velocity[x]            0.29242          2.1883         0.90807         0.90985
v  Velocity[y]           -0.38285           0.692      0.00056143      0.00034376
v  Velocity[z]           -0.42085         0.51047      -0.0012534      -0.0013743
v  TurbEner             0.0010211        0.014967       0.0032862       0.0033455
v  Dissip              9.2106e-05        0.030784      0.00045226       0.0003909
v  TurbVisc               0.16671          11.347          4.7126          5.2738
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              192:        0.96203E-01

===============================================================


 INSTANT    0.193000000E+03   TIME STEP NUMBER             193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000137E+04
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 :  0.23794E+00 0.12183E+01
   Friction velocity        uet   :  0.14234E-01 0.72614E-01
   Friction velocity        uk    :  0.17502E-01 0.38654E-01
   Dimensionless distance   yplus :  0.43034E+03 0.95272E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60019E+01      58   0.13371E-02   0.19673E-01 
c  VelocityX    0.46299E+04      12   0.67428E-02   0.42799E-03 
c  VelocityY    0.46299E+04      12   0.67428E-02   0.32219E-04 
c  VelocityZ    0.46299E+04      12   0.67428E-02   0.46510E-04 
c  TurbEner     0.59774E+01      13   0.11594E-03   0.15287E-08 
c  Dissip       0.15051E+01      16   0.18836E-02   0.40682E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.89           54523           26776           27270
v  Velocity[x]            0.29289          2.0199         0.90806         0.90983
v  Velocity[y]           -0.36738         0.70063      0.00056396      0.00034211
v  Velocity[z]           -0.42209         0.50427      -0.0012657      -0.0013828
v  TurbEner             0.0010231        0.015526       0.0032862       0.0033455
v  Dissip              9.2053e-05        0.032255      0.00045244      0.00039102
v  TurbVisc               0.16633          11.329          4.7126          5.2738
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              193:        0.96146E-01

===============================================================


 INSTANT    0.194000000E+03   TIME STEP NUMBER             194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002095E+04
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 :  0.23780E+00 0.13241E+01
   Friction velocity        uet   :  0.14225E-01 0.78922E-01
   Friction velocity        uk    :  0.17519E-01 0.38704E-01
   Dimensionless distance   yplus :  0.42996E+03 0.95269E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70287E+01      57   0.13448E-02   0.23042E-01 
c  VelocityX    0.46298E+04      12   0.63986E-02   0.28160E-03 
c  VelocityY    0.46298E+04      12   0.63986E-02   0.32939E-04 
c  VelocityZ    0.46298E+04      12   0.63986E-02   0.38687E-04 
c  TurbEner     0.59760E+01      14   0.13951E-03   0.21387E-08 
c  Dissip       0.14694E+01      16   0.20834E-02   0.67347E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.35           54532           26776           27270
v  Velocity[x]            0.29308          2.0815         0.90805         0.90982
v  Velocity[y]            -0.3822         0.69516      0.00056358      0.00034106
v  Velocity[z]           -0.41962         0.51178      -0.0012603      -0.0013799
v  TurbEner             0.0010227        0.014952       0.0032861       0.0033454
v  Dissip              9.2091e-05        0.030968      0.00045218      0.00039084
v  TurbVisc                0.1662          11.321          4.7125          5.2737
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              194:        0.95808E-01

===============================================================


 INSTANT    0.195000000E+03   TIME STEP NUMBER             195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001424E+04
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 :  0.23753E+00 0.12174E+01
   Friction velocity        uet   :  0.14209E-01 0.72575E-01
   Friction velocity        uk    :  0.17516E-01 0.38771E-01
   Dimensionless distance   yplus :  0.43028E+03 0.95287E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72153E+01      58   0.14866E-02   0.23651E-01 
c  VelocityX    0.46299E+04      12   0.66257E-02   0.34282E-03 
c  VelocityY    0.46299E+04      12   0.66257E-02   0.38130E-04 
c  VelocityZ    0.46299E+04      12   0.66257E-02   0.71896E-04 
c  TurbEner     0.59764E+01      13   0.66496E-04   0.92402E-09 
c  Dissip       0.14821E+01      13   0.42913E-03   0.34190E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.66           54540           26775           27269
v  Velocity[x]             0.2925          2.1543         0.90804         0.90982
v  Velocity[y]           -0.36605         0.70312       0.0005613      0.00034055
v  Velocity[z]            -0.4204         0.50652      -0.0012603      -0.0013793
v  TurbEner               0.00102        0.014801        0.003286       0.0033452
v  Dissip              9.2104e-05        0.030751      0.00045218      0.00039084
v  TurbVisc               0.16642          11.359          4.7125          5.2737
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              195:        0.95784E-01

===============================================================


 INSTANT    0.196000000E+03   TIME STEP NUMBER             196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001673E+04
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 :  0.23783E+00 0.13243E+01
   Friction velocity        uet   :  0.14227E-01 0.78940E-01
   Friction velocity        uk    :  0.17493E-01 0.38771E-01
   Dimensionless distance   yplus :  0.43010E+03 0.95262E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59722E+01      56   0.12622E-02   0.19585E-01 
c  VelocityX    0.46299E+04      12   0.69501E-02   0.34116E-03 
c  VelocityY    0.46299E+04      12   0.69501E-02   0.36046E-04 
c  VelocityZ    0.46299E+04      12   0.69501E-02   0.39028E-04 
c  TurbEner     0.59768E+01      12   0.67209E-04   0.80658E-09 
c  Dissip       0.15036E+01      15   0.93693E-03   0.19516E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.21           54550           26775           27270
v  Velocity[x]            0.29267          2.1782         0.90806         0.90984
v  Velocity[y]           -0.38234         0.69533      0.00055585      0.00033653
v  Velocity[z]           -0.42263         0.51104      -0.0012533      -0.0013715
v  TurbEner              0.001021        0.014919        0.003286       0.0033453
v  Dissip              9.2092e-05        0.031151      0.00045232      0.00039093
v  TurbVisc               0.16627          11.341          4.7124          5.2736
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              196:        0.95743E-01

===============================================================


 INSTANT    0.197000000E+03   TIME STEP NUMBER             197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999225E+04
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 :  0.23786E+00 0.12250E+01
   Friction velocity        uet   :  0.14228E-01 0.72550E-01
   Friction velocity        uk    :  0.17501E-01 0.38748E-01
   Dimensionless distance   yplus :  0.42949E+03 0.95207E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68700E+01      55   0.16808E-02   0.22518E-01 
c  VelocityX    0.46298E+04      12   0.72516E-02   0.41569E-03 
c  VelocityY    0.46298E+04      12   0.72516E-02   0.31327E-04 
c  VelocityZ    0.46298E+04      12   0.72516E-02   0.31475E-04 
c  TurbEner     0.59778E+01      13   0.10528E-03   0.95151E-09 
c  Dissip       0.15229E+01      16   0.19387E-02   0.43259E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.41           54540           26775           27269
v  Velocity[x]            0.29322          2.0284         0.90805         0.90983
v  Velocity[y]           -0.36778         0.70203      0.00056596      0.00034438
v  Velocity[z]           -0.41927         0.50416      -0.0012524      -0.0013709
v  TurbEner             0.0010225          0.0154       0.0032862       0.0033454
v  Dissip               9.209e-05        0.032656      0.00045256      0.00039111
v  TurbVisc                 0.166          11.345          4.7124          5.2736
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              197:        0.95507E-01

===============================================================


 INSTANT    0.198000000E+03   TIME STEP NUMBER             198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000079E+04
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 :  0.23751E+00 0.13260E+01
   Friction velocity        uet   :  0.14207E-01 0.79036E-01
   Friction velocity        uk    :  0.17515E-01 0.38730E-01
   Dimensionless distance   yplus :  0.43039E+03 0.95193E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57949E+01      60   0.14666E-02   0.19010E-01 
c  VelocityX    0.46298E+04      13   0.68172E-02   0.38325E-03 
c  VelocityY    0.46298E+04      13   0.68172E-02   0.28752E-04 
c  VelocityZ    0.46298E+04      13   0.68172E-02   0.44511E-04 
c  TurbEner     0.59763E+01      14   0.14642E-03   0.24360E-08 
c  Dissip       0.14863E+01      16   0.22455E-02   0.71810E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.45           54515           26777           27271
v  Velocity[x]             0.2929          2.0957         0.90805         0.90983
v  Velocity[y]           -0.38254         0.69513      0.00055892      0.00034099
v  Velocity[z]           -0.42098         0.51171      -0.0012464      -0.0013655
v  TurbEner             0.0010177         0.01475       0.0032859       0.0033453
v  Dissip               9.213e-05        0.031181      0.00045231      0.00039095
v  TurbVisc                0.1665          11.319          4.7124          5.2736
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              198:        0.97234E-01

===============================================================


 INSTANT    0.199000000E+03   TIME STEP NUMBER             199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997085E+04
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 :  0.23783E+00 0.12139E+01
   Friction velocity        uet   :  0.14226E-01 0.72358E-01
   Friction velocity        uk    :  0.17473E-01 0.38684E-01
   Dimensionless distance   yplus :  0.42973E+03 0.95130E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61297E+01      56   0.14003E-02   0.20087E-01 
c  VelocityX    0.46298E+04      12   0.69282E-02   0.33183E-03 
c  VelocityY    0.46298E+04      12   0.69282E-02   0.24379E-04 
c  VelocityZ    0.46298E+04      12   0.69282E-02   0.10631E-03 
c  TurbEner     0.59758E+01      12   0.60226E-04   0.82555E-09 
c  Dissip       0.14893E+01      13   0.32884E-03   0.22742E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.18           54521           26777           27271
v  Velocity[x]            0.29261          2.1443         0.90802          0.9098
v  Velocity[y]           -0.36648         0.70328      0.00056799      0.00034334
v  Velocity[z]            -0.4221         0.50604      -0.0012431      -0.0013645
v  TurbEner             0.0010196        0.014715       0.0032858       0.0033452
v  Dissip              9.2095e-05        0.031018      0.00045223      0.00039088
v  TurbVisc               0.16603          11.316          4.7123          5.2735
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              199:        0.95503E-01

===============================================================


 INSTANT    0.200000000E+03   TIME STEP NUMBER             200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999216E+04
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 :  0.23821E+00 0.13253E+01
   Friction velocity        uet   :  0.14248E-01 0.78997E-01
   Friction velocity        uk    :  0.17489E-01 0.38725E-01
   Dimensionless distance   yplus :  0.42932E+03 0.95144E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62782E+01      56   0.12794E-02   0.20581E-01 
c  VelocityX    0.46298E+04      12   0.69807E-02   0.37106E-03 
c  VelocityY    0.46298E+04      12   0.69807E-02   0.34924E-04 
c  VelocityZ    0.46298E+04      12   0.69807E-02   0.47036E-04 
c  TurbEner     0.59766E+01      13   0.82182E-04   0.10008E-08 
c  Dissip       0.15055E+01      15   0.81236E-03   0.16661E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -165.34           54523           26777           27272
v  Velocity[x]            0.29275          2.1721         0.90805         0.90983
v  Velocity[y]           -0.38219         0.69258      0.00055472      0.00033608
v  Velocity[z]            -0.4212         0.51112      -0.0012521      -0.0013748
v  TurbEner             0.0010194        0.014814       0.0032858       0.0033452
v  Dissip              9.2097e-05        0.031146      0.00045231      0.00039093
v  TurbVisc               0.16586          11.347          4.7123          5.2735
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              200:        0.95797E-01

===============================================================


 INSTANT    0.201000000E+03   TIME STEP NUMBER             201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998103E+04
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 :  0.23786E+00 0.12268E+01
   Friction velocity        uet   :  0.14227E-01 0.72557E-01
   Friction velocity        uk    :  0.17487E-01 0.38740E-01
   Dimensionless distance   yplus :  0.42972E+03 0.95193E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71057E+01      57   0.16691E-02   0.23302E-01 
c  VelocityX    0.46299E+04      13   0.62805E-02   0.39796E-03 
c  VelocityY    0.46299E+04      13   0.62805E-02   0.42036E-04 
c  VelocityZ    0.46299E+04      13   0.62805E-02   0.28319E-04 
c  TurbEner     0.59769E+01      13   0.11350E-03   0.11949E-08 
c  Dissip       0.15176E+01      15   0.17799E-02   0.33653E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.04           54504           26777           27271
v  Velocity[x]            0.29288          2.0274         0.90804         0.90982
v  Velocity[y]           -0.36695         0.70081      0.00056177      0.00034103
v  Velocity[z]           -0.42292         0.50473        -0.00125      -0.0013717
v  TurbEner             0.0010164        0.015319       0.0032857       0.0033451
v  Dissip              9.2106e-05        0.032534      0.00045246      0.00039104
v  TurbVisc               0.16609          11.333          4.7122          5.2734
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              201:        0.96548E-01

===============================================================


 INSTANT    0.202000000E+03   TIME STEP NUMBER             202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001953E+04
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 :  0.23748E+00 0.13245E+01
   Friction velocity        uet   :  0.14204E-01 0.78948E-01
   Friction velocity        uk    :  0.17462E-01 0.38735E-01
   Dimensionless distance   yplus :  0.42944E+03 0.95202E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61495E+01      53   0.12516E-02   0.20167E-01 
c  VelocityX    0.46298E+04      12   0.66939E-02   0.30884E-03 
c  VelocityY    0.46298E+04      12   0.66939E-02   0.28343E-04 
c  VelocityZ    0.46298E+04      12   0.66939E-02   0.41183E-04 
c  TurbEner     0.59747E+01      13   0.13303E-03   0.19673E-08 
c  Dissip       0.14821E+01      16   0.21920E-02   0.65771E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.51           54516           26777           27271
v  Velocity[x]             0.2926          2.0912         0.90805         0.90982
v  Velocity[y]           -0.38237          0.6932      0.00055221      0.00033217
v  Velocity[z]           -0.42149         0.51172      -0.0012544      -0.0013756
v  TurbEner             0.0010173         0.01474       0.0032854       0.0033449
v  Dissip              9.2061e-05        0.031076      0.00045215      0.00039082
v  TurbVisc               0.16586          11.344          4.7121          5.2733
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              202:        0.95502E-01

===============================================================


 INSTANT    0.203000000E+03   TIME STEP NUMBER             203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999390E+04
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 :  0.23795E+00 0.12412E+01
   Friction velocity        uet   :  0.14232E-01 0.72531E-01
   Friction velocity        uk    :  0.17469E-01 0.38677E-01
   Dimensionless distance   yplus :  0.42875E+03 0.95232E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60689E+01      57   0.12666E-02   0.19886E-01 
c  VelocityX    0.46298E+04      12   0.72618E-02   0.31409E-03 
c  VelocityY    0.46298E+04      12   0.72618E-02   0.22412E-04 
c  VelocityZ    0.46298E+04      12   0.72618E-02   0.52009E-04 
c  TurbEner     0.59747E+01      12   0.58543E-04   0.62836E-09 
c  Dissip       0.14835E+01      13   0.32822E-03   0.19157E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.43           54530           26776           27270
v  Velocity[x]             0.2931          2.1433         0.90805         0.90983
v  Velocity[y]            -0.3668         0.70129      0.00055788      0.00033549
v  Velocity[z]           -0.42052         0.50573       -0.001255      -0.0013765
v  TurbEner             0.0010188         0.01472       0.0032851       0.0033447
v  Dissip              9.2058e-05        0.030909      0.00045204      0.00039074
v  TurbVisc               0.16553          11.382          4.7119          5.2732
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              203:        0.95912E-01

===============================================================


 INSTANT    0.204000000E+03   TIME STEP NUMBER             204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001615E+04
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 :  0.23731E+00 0.13240E+01
   Friction velocity        uet   :  0.14194E-01 0.78914E-01
   Friction velocity        uk    :  0.17483E-01 0.38710E-01
   Dimensionless distance   yplus :  0.42952E+03 0.95303E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58945E+01      55   0.11469E-02   0.19323E-01 
c  VelocityX    0.46299E+04      12   0.73430E-02   0.30631E-03 
c  VelocityY    0.46299E+04      12   0.73430E-02   0.24682E-04 
c  VelocityZ    0.46299E+04      12   0.73430E-02   0.53930E-04 
c  TurbEner     0.59757E+01      13   0.72351E-04   0.84992E-09 
c  Dissip       0.14992E+01      15   0.68865E-03   0.11730E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.05           54542           26776           27270
v  Velocity[x]            0.29267          2.1771         0.90807         0.90984
v  Velocity[y]           -0.38284         0.69339      0.00054094      0.00032027
v  Velocity[z]           -0.41989         0.51044      -0.0012645      -0.0013842
v  TurbEner             0.0010149        0.014814       0.0032851       0.0033447
v  Dissip              9.2039e-05        0.030991      0.00045211      0.00039077
v  TurbVisc               0.16596          11.362          4.7118          5.2731
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              204:        0.95161E-01

===============================================================


 INSTANT    0.205000000E+03   TIME STEP NUMBER             205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000607E+04
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 :  0.23814E+00 0.12347E+01
   Friction velocity        uet   :  0.14244E-01 0.72480E-01
   Friction velocity        uk    :  0.17449E-01 0.38663E-01
   Dimensionless distance   yplus :  0.42899E+03 0.95327E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68617E+01      65   0.15165E-02   0.22473E-01 
c  VelocityX    0.46298E+04      13   0.73277E-02   0.42713E-03 
c  VelocityY    0.46298E+04      13   0.73277E-02   0.61120E-04 
c  VelocityZ    0.46298E+04      13   0.73277E-02   0.12135E-03 
c  TurbEner     0.59771E+01      13   0.77025E-04   0.88491E-09 
c  Dissip       0.15258E+01      15   0.78569E-03   0.11657E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.64           54546           26775           27269
v  Velocity[x]            0.29276          2.2117         0.90807         0.90984
v  Velocity[y]           -0.36744         0.70035      0.00056004      0.00033561
v  Velocity[z]           -0.42194         0.50425      -0.0012563       -0.001377
v  TurbEner             0.0010175        0.015041       0.0032853       0.0033448
v  Dissip               9.208e-05        0.031458      0.00045228      0.00039088
v  TurbVisc               0.16557          11.362          4.7119          5.2731
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              205:        0.97534E-01

===============================================================


 INSTANT    0.206000000E+03   TIME STEP NUMBER             206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001981E+04
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 :  0.23777E+00 0.13249E+01
   Friction velocity        uet   :  0.14221E-01 0.78968E-01
   Friction velocity        uk    :  0.17472E-01 0.38688E-01
   Dimensionless distance   yplus :  0.42879E+03 0.95367E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.77598E+01      58   0.19745E-02   0.25446E-01 
c  VelocityX    0.46297E+04      12   0.72616E-02   0.85946E-03 
c  VelocityY    0.46297E+04      12   0.72616E-02   0.31186E-04 
c  VelocityZ    0.46297E+04      12   0.72616E-02   0.62608E-04 
c  TurbEner     0.59774E+01      14   0.23175E-03   0.33169E-08 
c  Dissip       0.15240E+01      17   0.40596E-02   0.15734E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.59           54539           26775           27270
v  Velocity[x]            0.29306          1.6236         0.90806         0.90983
v  Velocity[y]           -0.38227         0.69468      0.00054212      0.00032371
v  Velocity[z]           -0.42177         0.51182      -0.0012622      -0.0013795
v  TurbEner             0.0010181        0.016258       0.0032857        0.003345
v  Dissip              9.2106e-05        0.034713      0.00045254       0.0003911
v  TurbVisc               0.16548          11.335          4.7119          5.2731
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              206:        0.96317E-01

===============================================================


 INSTANT    0.207000000E+03   TIME STEP NUMBER             207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999326E+04
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 :  0.23754E+00 0.12454E+01
   Friction velocity        uet   :  0.14207E-01 0.72431E-01
   Friction velocity        uk    :  0.17476E-01 0.38720E-01
   Dimensionless distance   yplus :  0.42932E+03 0.95373E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68403E+01      69   0.16183E-02   0.22435E-01 
c  VelocityX    0.46296E+04      12   0.68823E-02   0.40577E-03 
c  VelocityY    0.46296E+04      12   0.68823E-02   0.30110E-04 
c  VelocityZ    0.46296E+04      12   0.68823E-02   0.47981E-04 
c  TurbEner     0.59711E+01      16   0.52583E-03   0.16392E-07 
c  Dissip       0.13272E+01      19   0.10956E-01   0.91564E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.93           54516           26775           27269
v  Velocity[x]            0.29279          1.8033         0.90806         0.90983
v  Velocity[y]           -0.36614         0.70232      0.00055646      0.00033757
v  Velocity[z]           -0.42144         0.50642      -0.0012541      -0.0013709
v  TurbEner             0.0010153        0.013431       0.0032852       0.0033447
v  Dissip              9.2092e-05        0.027408      0.00045152      0.00039037
v  TurbVisc               0.16574           11.33           4.712          5.2732
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              207:        0.99673E-01

===============================================================


 INSTANT    0.208000000E+03   TIME STEP NUMBER             208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000368E+04
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 :  0.23784E+00 0.13251E+01
   Friction velocity        uet   :  0.14226E-01 0.78985E-01
   Friction velocity        uk    :  0.17453E-01 0.38740E-01
   Dimensionless distance   yplus :  0.42911E+03 0.95391E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60454E+01      54   0.12434E-02   0.19825E-01 
c  VelocityX    0.46297E+04      12   0.70737E-02   0.39431E-03 
c  VelocityY    0.46297E+04      12   0.70737E-02   0.25590E-04 
c  VelocityZ    0.46297E+04      12   0.70737E-02   0.46020E-04 
c  TurbEner     0.59684E+01      14   0.21283E-03   0.44393E-08 
c  Dissip       0.12479E+01      19   0.52491E-02   0.25482E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.07           54526           26776           27270
v  Velocity[x]            0.29259          1.9445         0.90804         0.90981
v  Velocity[y]           -0.38228         0.69342      0.00054836      0.00032907
v  Velocity[z]           -0.42281         0.51118      -0.0012622      -0.0013814
v  TurbEner             0.0010162        0.012433       0.0032847       0.0033444
v  Dissip              9.2071e-05        0.024282      0.00045056      0.00038969
v  TurbVisc               0.16547          11.354          4.7119           5.273
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              208:        0.95972E-01

===============================================================


 INSTANT    0.209000000E+03   TIME STEP NUMBER             209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998354E+04
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 :  0.23776E+00 0.12160E+01
   Friction velocity        uet   :  0.14221E-01 0.72484E-01
   Friction velocity        uk    :  0.17460E-01 0.38746E-01
   Dimensionless distance   yplus :  0.42842E+03 0.95359E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70021E+01      56   0.13050E-02   0.22947E-01 
c  VelocityX    0.46298E+04      12   0.68754E-02   0.36493E-03 
c  VelocityY    0.46298E+04      12   0.68754E-02   0.41624E-04 
c  VelocityZ    0.46298E+04      12   0.68754E-02   0.87645E-04 
c  TurbEner     0.59678E+01      13   0.96097E-04   0.15099E-08 
c  Dissip       0.12156E+01      18   0.25467E-02   0.81080E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.61           54534           26775           27269
v  Velocity[x]             0.2927          2.0486         0.90803         0.90981
v  Velocity[y]           -0.36773         0.70054      0.00056137      0.00033807
v  Velocity[z]            -0.4194         0.50419      -0.0012433      -0.0013603
v  TurbEner             0.0010179        0.012232       0.0032843        0.003344
v  Dissip              9.2098e-05        0.022959      0.00044976      0.00038914
v  TurbVisc                0.1651          11.335          4.7119          5.2731
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              209:        0.96280E-01

===============================================================


 INSTANT    0.210000000E+03   TIME STEP NUMBER             210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001756E+04
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 :  0.23767E+00 0.13244E+01
   Friction velocity        uet   :  0.14216E-01 0.78938E-01
   Friction velocity        uk    :  0.17474E-01 0.38787E-01
   Dimensionless distance   yplus :  0.42930E+03 0.95335E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70696E+01      55   0.15278E-02   0.23193E-01 
c  VelocityX    0.46297E+04      13   0.64348E-02   0.33456E-03 
c  VelocityY    0.46297E+04      13   0.64348E-02   0.41314E-04 
c  VelocityZ    0.46297E+04      13   0.64348E-02   0.44817E-04 
c  TurbEner     0.59682E+01      13   0.77869E-04   0.97728E-09 
c  Dissip       0.11960E+01      17   0.12677E-02   0.30237E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.76           54541           26776           27270
v  Velocity[x]            0.29277          2.0966         0.90805         0.90983
v  Velocity[y]           -0.38238         0.69245       0.0005504      0.00032933
v  Velocity[z]             -0.421         0.51172      -0.0012564      -0.0013778
v  TurbEner             0.0010135        0.012477        0.003284       0.0033439
v  Dissip              9.2102e-05        0.022548      0.00044913      0.00038871
v  TurbVisc               0.16554          11.344          4.7119          5.2731
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              210:        0.96725E-01

===============================================================


 INSTANT    0.211000000E+03   TIME STEP NUMBER             211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998712E+04
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 :  0.23773E+00 0.12157E+01
   Friction velocity        uet   :  0.14221E-01 0.72466E-01
   Friction velocity        uk    :  0.17437E-01 0.38708E-01
   Dimensionless distance   yplus :  0.42872E+03 0.95352E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62974E+01      57   0.12399E-02   0.20634E-01 
c  VelocityX    0.46299E+04      12   0.70817E-02   0.30736E-03 
c  VelocityY    0.46299E+04      12   0.70817E-02   0.28010E-04 
c  VelocityZ    0.46299E+04      12   0.70817E-02   0.28553E-04 
c  TurbEner     0.59692E+01      13   0.82701E-04   0.97792E-09 
c  Dissip       0.11992E+01      16   0.48967E-03   0.71035E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.18           54549           26775           27269
v  Velocity[x]             0.2929          2.1512         0.90804         0.90982
v  Velocity[y]           -0.36655         0.70026      0.00055664      0.00033478
v  Velocity[z]           -0.42249         0.50603      -0.0012513      -0.0013714
v  TurbEner             0.0010152        0.012841       0.0032838       0.0033438
v  Dissip              9.2081e-05        0.022663      0.00044868       0.0003884
v  TurbVisc               0.16505          11.326          4.7121          5.2732
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              211:        0.96148E-01

===============================================================


 INSTANT    0.212000000E+03   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001813E+04
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 :  0.23778E+00 0.13235E+01
   Friction velocity        uet   :  0.14224E-01 0.78896E-01
   Friction velocity        uk    :  0.17452E-01 0.38726E-01
   Dimensionless distance   yplus :  0.42831E+03 0.95362E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63029E+01      55   0.16218E-02   0.20657E-01 
c  VelocityX    0.46298E+04      12   0.75904E-02   0.39779E-03 
c  VelocityY    0.46298E+04      12   0.75904E-02   0.27724E-04 
c  VelocityZ    0.46298E+04      12   0.75904E-02   0.51400E-04 
c  TurbEner     0.59706E+01      14   0.14306E-03   0.21415E-08 
c  Dissip       0.12060E+01      16   0.17273E-02   0.28661E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.93           54540           26775           27270
v  Velocity[x]            0.29276           1.993         0.90807         0.90985
v  Velocity[y]           -0.38227         0.69312      0.00055019      0.00033204
v  Velocity[z]           -0.41983         0.51106      -0.0012596      -0.0013782
v  TurbEner             0.0010142        0.013652       0.0032841        0.003344
v  Dissip              9.2077e-05        0.023912      0.00044844      0.00038826
v  TurbVisc               0.16487          11.324          4.7122          5.2733
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              212:        0.95975E-01

===============================================================


 INSTANT    0.213000000E+03   TIME STEP NUMBER             213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998982E+04
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 :  0.23760E+00 0.12416E+01
   Friction velocity        uet   :  0.14213E-01 0.72465E-01
   Friction velocity        uk    :  0.17443E-01 0.38782E-01
   Dimensionless distance   yplus :  0.42851E+03 0.95362E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68394E+01      60   0.15241E-02   0.22433E-01 
c  VelocityX    0.46299E+04      12   0.66648E-02   0.47352E-03 
c  VelocityY    0.46299E+04      12   0.66648E-02   0.34686E-04 
c  VelocityZ    0.46299E+04      12   0.66648E-02   0.10343E-03 
c  TurbEner     0.59708E+01      13   0.83661E-04   0.12339E-08 
c  Dissip       0.11879E+01      17   0.14873E-02   0.33829E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.15           54513           26775           27269
v  Velocity[x]            0.29245          2.0734         0.90808         0.90985
v  Velocity[y]           -0.36705         0.70061      0.00055719      0.00033775
v  Velocity[z]           -0.42065         0.50469      -0.0012498      -0.0013677
v  TurbEner             0.0010106        0.013452       0.0032842       0.0033441
v  Dissip              9.2083e-05        0.023099      0.00044805        0.000388
v  TurbVisc               0.16496          11.358          4.7125          5.2736
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              213:        0.95978E-01

===============================================================


 INSTANT    0.214000000E+03   TIME STEP NUMBER             214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000772E+04
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 :  0.23775E+00 0.13250E+01
   Friction velocity        uet   :  0.14223E-01 0.78981E-01
   Friction velocity        uk    :  0.17412E-01 0.38828E-01
   Dimensionless distance   yplus :  0.42819E+03 0.95379E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54778E+01      54   0.11942E-02   0.17960E-01 
c  VelocityX    0.46299E+04      12   0.64635E-02   0.35765E-03 
c  VelocityY    0.46299E+04      12   0.64635E-02   0.27592E-04 
c  VelocityZ    0.46299E+04      12   0.64635E-02   0.48716E-04 
c  TurbEner     0.59712E+01      13   0.81980E-04   0.14628E-08 
c  Dissip       0.11975E+01      15   0.51303E-03   0.66762E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.69           54522           26776           27270
v  Velocity[x]            0.29278          2.1278         0.90806         0.90983
v  Velocity[y]           -0.38251         0.69462      0.00054913       0.0003298
v  Velocity[z]           -0.42294         0.51177      -0.0012541      -0.0013724
v  TurbEner             0.0010105        0.013657       0.0032843       0.0033442
v  Dissip              9.2097e-05        0.023233      0.00044785      0.00038786
v  TurbVisc               0.16467          11.342          4.7127          5.2738
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              214:        0.95827E-01

===============================================================


 INSTANT    0.215000000E+03   TIME STEP NUMBER             215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997450E+04
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 :  0.23783E+00 0.12144E+01
   Friction velocity        uet   :  0.14227E-01 0.72309E-01
   Friction velocity        uk    :  0.17411E-01 0.38842E-01
   Dimensionless distance   yplus :  0.42738E+03 0.95388E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56632E+01      52   0.11736E-02   0.18556E-01 
c  VelocityX    0.46300E+04      12   0.70099E-02   0.26794E-03 
c  VelocityY    0.46300E+04      12   0.70099E-02   0.22492E-04 
c  VelocityZ    0.46300E+04      12   0.70099E-02   0.31698E-04 
c  TurbEner     0.59729E+01      13   0.10249E-03   0.17637E-08 
c  Dissip       0.12239E+01      16   0.11414E-02   0.24787E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.2           54531           26776           27270
v  Velocity[x]            0.29313          2.1676         0.90804         0.90983
v  Velocity[y]           -0.36693          0.7024      0.00055575       0.0003336
v  Velocity[z]           -0.42169         0.50566      -0.0012556      -0.0013735
v  TurbEner             0.0010116        0.013996       0.0032846       0.0033444
v  Dissip              9.2082e-05        0.023826      0.00044791       0.0003879
v  TurbVisc               0.16436          11.344           4.713           5.274
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              215:        0.95202E-01

===============================================================


 INSTANT    0.216000000E+03   TIME STEP NUMBER             216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001124E+04
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 :  0.23788E+00 0.13256E+01
   Friction velocity        uet   :  0.14230E-01 0.79019E-01
   Friction velocity        uk    :  0.17421E-01 0.38824E-01
   Dimensionless distance   yplus :  0.42816E+03 0.95398E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64174E+01      61   0.13755E-02   0.21058E-01 
c  VelocityX    0.46300E+04      12   0.71230E-02   0.35945E-03 
c  VelocityY    0.46300E+04      12   0.71230E-02   0.34222E-04 
c  VelocityZ    0.46300E+04      12   0.71230E-02   0.37596E-04 
c  TurbEner     0.59741E+01      14   0.13273E-03   0.22279E-08 
c  Dissip       0.12464E+01      17   0.21580E-02   0.56966E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.14           54541           26776           27270
v  Velocity[x]            0.29258          1.9978         0.90807         0.90985
v  Velocity[y]           -0.38286         0.69191      0.00054345      0.00032579
v  Velocity[z]            -0.4216         0.51051      -0.0012678      -0.0013849
v  TurbEner             0.0010068        0.014744       0.0032849       0.0033447
v  Dissip              9.2116e-05        0.025429      0.00044811      0.00038804
v  TurbVisc               0.16487          11.319          4.7133          5.2743
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              216:        0.96896E-01

===============================================================


 INSTANT    0.217000000E+03   TIME STEP NUMBER             217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999014E+04
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 :  0.23789E+00 0.12326E+01
   Friction velocity        uet   :  0.14231E-01 0.72569E-01
   Friction velocity        uk    :  0.17379E-01 0.38723E-01
   Dimensionless distance   yplus :  0.42748E+03 0.95399E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67924E+01      62   0.13852E-02   0.22259E-01 
c  VelocityX    0.46301E+04      12   0.67049E-02   0.35570E-03 
c  VelocityY    0.46301E+04      12   0.67049E-02   0.54932E-04 
c  VelocityZ    0.46301E+04      12   0.67049E-02   0.11571E-03 
c  TurbEner     0.59742E+01      13   0.94017E-04   0.14501E-08 
c  Dissip       0.12391E+01      16   0.11822E-02   0.24117E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.82           54550           26775           27270
v  Velocity[x]            0.29274          2.0841         0.90805         0.90983
v  Velocity[y]           -0.36743         0.69992      0.00055996      0.00033596
v  Velocity[z]           -0.42204         0.50429       -0.001245      -0.0013646
v  TurbEner             0.0010092        0.014375       0.0032851       0.0033448
v  Dissip              9.2182e-05        0.024768      0.00044804        0.000388
v  TurbVisc               0.16454          11.327          4.7135          5.2745
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              217:        0.98675E-01

===============================================================


 INSTANT    0.218000000E+03   TIME STEP NUMBER             218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002205E+04
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 :  0.23789E+00 0.13238E+01
   Friction velocity        uet   :  0.14230E-01 0.78904E-01
   Friction velocity        uk    :  0.17400E-01 0.38743E-01
   Dimensionless distance   yplus :  0.42713E+03 0.95389E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68076E+01      59   0.16044E-02   0.22313E-01 
c  VelocityX    0.46301E+04      12   0.72013E-02   0.40302E-03 
c  VelocityY    0.46301E+04      12   0.72013E-02   0.46267E-04 
c  VelocityZ    0.46301E+04      12   0.72013E-02   0.58431E-04 
c  TurbEner     0.59752E+01      13   0.73093E-04   0.87952E-09 
c  Dissip       0.12531E+01      15   0.59229E-03   0.91605E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.15           54541           26776           27270
v  Velocity[x]            0.29296          2.1305         0.90808         0.90986
v  Velocity[y]           -0.38225         0.69315      0.00055155      0.00033275
v  Velocity[z]           -0.42054         0.51181      -0.0012505        -0.00137
v  TurbEner             0.0010102        0.014427       0.0032856       0.0033452
v  Dissip               9.221e-05        0.024917       0.0004482      0.00038811
v  TurbVisc               0.16458          11.365          4.7138          5.2747
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              218:        0.96260E-01

===============================================================


 INSTANT    0.219000000E+03   TIME STEP NUMBER             219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998167E+04
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 :  0.23733E+00 0.12163E+01
   Friction velocity        uet   :  0.14196E-01 0.72507E-01
   Friction velocity        uk    :  0.17409E-01 0.38813E-01
   Dimensionless distance   yplus :  0.42769E+03 0.95385E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68403E+01      54   0.15379E-02   0.22434E-01 
c  VelocityX    0.46304E+04      12   0.70143E-02   0.36568E-03 
c  VelocityY    0.46304E+04      12   0.70143E-02   0.40766E-04 
c  VelocityZ    0.46304E+04      12   0.70143E-02   0.33870E-04 
c  TurbEner     0.59772E+01      13   0.92236E-04   0.15940E-08 
c  Dissip       0.12834E+01      16   0.11828E-02   0.30030E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.46           54517           26776           27270
v  Velocity[x]            0.29274          2.1755         0.90807         0.90985
v  Velocity[y]           -0.36613         0.70163      0.00055654      0.00033879
v  Velocity[z]           -0.42157         0.50649      -0.0012392      -0.0013572
v  TurbEner             0.0010092        0.014631        0.003286       0.0033455
v  Dissip               9.218e-05        0.025513      0.00044854      0.00038835
v  TurbVisc               0.16511          11.348          4.7142          5.2751
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              219:        0.95511E-01

===============================================================


 INSTANT    0.220000000E+03   TIME STEP NUMBER             220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999423E+04
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 :  0.23765E+00 0.13233E+01
   Friction velocity        uet   :  0.14215E-01 0.78876E-01
   Friction velocity        uk    :  0.17400E-01 0.38865E-01
   Dimensionless distance   yplus :  0.42773E+03 0.95401E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64060E+01      59   0.14708E-02   0.21018E-01 
c  VelocityX    0.46302E+04      12   0.69470E-02   0.47375E-03 
c  VelocityY    0.46302E+04      12   0.69470E-02   0.31904E-04 
c  VelocityZ    0.46302E+04      12   0.69470E-02   0.44840E-04 
c  TurbEner     0.59771E+01      13   0.12247E-03   0.20215E-08 
c  Dissip       0.13072E+01      17   0.21844E-02   0.60361E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.57           54527           26778           27272
v  Velocity[x]            0.29266          2.0066         0.90806         0.90984
v  Velocity[y]           -0.38234         0.69471      0.00055057      0.00033283
v  Velocity[z]           -0.42162         0.51108      -0.0012538      -0.0013746
v  TurbEner             0.0010125        0.015302       0.0032864       0.0033458
v  Dissip              9.2162e-05        0.027196      0.00044891       0.0003886
v  TurbVisc               0.16527          11.351          4.7145          5.2754
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              220:        0.96585E-01

===============================================================


 INSTANT    0.221000000E+03   TIME STEP NUMBER             221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997696E+04
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 :  0.23812E+00 0.12317E+01
   Friction velocity        uet   :  0.14243E-01 0.72518E-01
   Friction velocity        uk    :  0.17428E-01 0.38792E-01
   Dimensionless distance   yplus :  0.42746E+03 0.95327E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61490E+01      55   0.12925E-02   0.20156E-01 
c  VelocityX    0.46303E+04      12   0.60963E-02   0.35816E-03 
c  VelocityY    0.46303E+04      12   0.60963E-02   0.28908E-04 
c  VelocityZ    0.46303E+04      12   0.60963E-02   0.96518E-04 
c  TurbEner     0.59763E+01      14   0.11047E-03   0.18815E-08 
c  Dissip       0.12983E+01      16   0.12151E-02   0.27716E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.25           54535           26777           27271
v  Velocity[x]            0.29303           2.085         0.90804         0.90983
v  Velocity[y]           -0.36778         0.70113      0.00056201      0.00033688
v  Velocity[z]           -0.42082         0.50416      -0.0012427      -0.0013629
v  TurbEner             0.0010169        0.014857       0.0032865       0.0033458
v  Dissip              9.2172e-05         0.02653      0.00044894      0.00038861
v  TurbVisc               0.16538          11.324          4.7147          5.2756
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              221:        0.96198E-01

===============================================================


 INSTANT    0.222000000E+03   TIME STEP NUMBER             222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001208E+04
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 :  0.23771E+00 0.13260E+01
   Friction velocity        uet   :  0.14218E-01 0.79041E-01
   Friction velocity        uk    :  0.17467E-01 0.38788E-01
   Dimensionless distance   yplus :  0.42881E+03 0.95217E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57632E+01      54   0.12981E-02   0.18909E-01 
c  VelocityX    0.46303E+04      13   0.61458E-02   0.29323E-03 
c  VelocityY    0.46303E+04      13   0.61458E-02   0.28119E-04 
c  VelocityZ    0.46303E+04      13   0.61458E-02   0.47062E-04 
c  TurbEner     0.59769E+01      12   0.62074E-04   0.57960E-09 
c  Dissip       0.13141E+01      15   0.54448E-03   0.80373E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.48           54545           26778           27272
v  Velocity[x]            0.29256          2.1335         0.90807         0.90985
v  Velocity[y]           -0.38252         0.69458      0.00055067       0.0003287
v  Velocity[z]           -0.42252         0.51174      -0.0012558      -0.0013743
v  TurbEner             0.0010163        0.014807       0.0032867        0.003346
v  Dissip              9.2098e-05        0.026645       0.0004492      0.00038878
v  TurbVisc               0.16636          11.306          4.7148          5.2757
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              222:        0.96275E-01

===============================================================


 INSTANT    0.223000000E+03   TIME STEP NUMBER             223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998713E+04
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 :  0.23762E+00 0.12137E+01
   Friction velocity        uet   :  0.14212E-01 0.72329E-01
   Friction velocity        uk    :  0.17461E-01 0.38704E-01
   Dimensionless distance   yplus :  0.42895E+03 0.95129E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60719E+01      57   0.13027E-02   0.19903E-01 
c  VelocityX    0.46304E+04      12   0.71760E-02   0.32063E-03 
c  VelocityY    0.46304E+04      12   0.71760E-02   0.23614E-04 
c  VelocityZ    0.46304E+04      12   0.71760E-02   0.26698E-04 
c  TurbEner     0.59780E+01      12   0.68232E-04   0.77132E-09 
c  Dissip       0.13436E+01      16   0.10988E-02   0.26398E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.35           54553           26778           27272
v  Velocity[x]            0.29293          2.1732         0.90806         0.90984
v  Velocity[y]           -0.36652          0.7026      0.00055962      0.00033748
v  Velocity[z]           -0.42155         0.50602      -0.0012571      -0.0013751
v  TurbEner             0.0010228        0.014934        0.003287       0.0033461
v  Dissip              9.2045e-05          0.0272      0.00044956        0.000389
v  TurbVisc               0.16656          11.345           4.715          5.2759
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              223:        0.95792E-01

===============================================================


 INSTANT    0.224000000E+03   TIME STEP NUMBER             224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999803E+04
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 :  0.23794E+00 0.13252E+01
   Friction velocity        uet   :  0.14231E-01 0.78991E-01
   Friction velocity        uk    :  0.17517E-01 0.38745E-01
   Dimensionless distance   yplus :  0.42947E+03 0.95099E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64930E+01      59   0.14940E-02   0.21284E-01 
c  VelocityX    0.46303E+04      12   0.76005E-02   0.40078E-03 
c  VelocityY    0.46303E+04      12   0.76005E-02   0.46956E-04 
c  VelocityZ    0.46303E+04      12   0.76005E-02   0.33696E-04 
c  TurbEner     0.59789E+01      13   0.11607E-03   0.14874E-08 
c  Dissip       0.13671E+01      16   0.20784E-02   0.53880E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.12           54544           26778           27272
v  Velocity[x]            0.29307          2.0027         0.90807         0.90985
v  Velocity[y]           -0.38223         0.69264      0.00055876      0.00033907
v  Velocity[z]            -0.4201         0.51111      -0.0012578      -0.0013764
v  TurbEner             0.0010275        0.015528       0.0032875       0.0033465
v  Dissip              9.1992e-05        0.028828      0.00044999      0.00038929
v  TurbVisc               0.16711          11.333          4.7152           5.276
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              224:        0.96158E-01

===============================================================


 INSTANT    0.225000000E+03   TIME STEP NUMBER             225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998984E+04
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 :  0.23724E+00 0.12183E+01
   Friction velocity        uet   :  0.14189E-01 0.72533E-01
   Friction velocity        uk    :  0.17557E-01 0.38783E-01
   Dimensionless distance   yplus :  0.43086E+03 0.95102E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68975E+01      58   0.15333E-02   0.22633E-01 
c  VelocityX    0.46305E+04      13   0.73025E-02   0.44991E-03 
c  VelocityY    0.46305E+04      13   0.73025E-02   0.26689E-04 
c  VelocityZ    0.46305E+04      13   0.73025E-02   0.56171E-04 
c  TurbEner     0.59783E+01      14   0.12230E-03   0.21914E-08 
c  Dissip       0.13484E+01      16   0.15284E-02   0.40236E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.49           54519           26779           27273
v  Velocity[x]            0.29274          2.0829         0.90808         0.90986
v  Velocity[y]           -0.36696         0.70024      0.00055632      0.00033656
v  Velocity[z]           -0.42015         0.50477       -0.001256       -0.001372
v  TurbEner             0.0010295        0.014968       0.0032877       0.0033467
v  Dissip              9.2013e-05          0.0279      0.00045005      0.00038934
v  TurbVisc               0.16809          11.333          4.7154          5.2763
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              225:        0.97051E-01

===============================================================


 INSTANT    0.226000000E+03   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998448E+04
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 :  0.23796E+00 0.13244E+01
   Friction velocity        uet   :  0.14232E-01 0.78949E-01
   Friction velocity        uk    :  0.17574E-01 0.38768E-01
   Dimensionless distance   yplus :  0.43164E+03 0.95139E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61986E+01      53   0.12097E-02   0.20316E-01 
c  VelocityX    0.46304E+04      12   0.65909E-02   0.39884E-03 
c  VelocityY    0.46304E+04      12   0.65909E-02   0.25372E-04 
c  VelocityZ    0.46304E+04      12   0.65909E-02   0.42630E-04 
c  TurbEner     0.59781E+01      13   0.72300E-04   0.10772E-08 
c  Dissip       0.13617E+01      14   0.37138E-03   0.41543E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.52           54525           26779           27273
v  Velocity[x]            0.29255          2.1337         0.90808         0.90985
v  Velocity[y]            -0.3824         0.69558      0.00055465      0.00033342
v  Velocity[z]           -0.42168         0.51175      -0.0012631      -0.0013823
v  TurbEner             0.0010353        0.014862        0.003288       0.0033468
v  Dissip              9.2006e-05         0.02788      0.00045022      0.00038944
v  TurbVisc               0.16862          11.364          4.7156          5.2764
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              226:        0.95194E-01

===============================================================


 INSTANT    0.227000000E+03   TIME STEP NUMBER             227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998515E+04
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 :  0.23794E+00 0.12375E+01
   Friction velocity        uet   :  0.14231E-01 0.72347E-01
   Friction velocity        uk    :  0.17623E-01 0.38739E-01
   Dimensionless distance   yplus :  0.43191E+03 0.95209E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71543E+01      61   0.15647E-02   0.23451E-01 
c  VelocityX    0.46305E+04      12   0.72717E-02   0.36810E-03 
c  VelocityY    0.46305E+04      12   0.72717E-02   0.43934E-04 
c  VelocityZ    0.46305E+04      12   0.72717E-02   0.78999E-04 
c  TurbEner     0.59794E+01      13   0.85889E-04   0.12344E-08 
c  Dissip       0.13911E+01      16   0.87164E-03   0.18778E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.02           54540           26778           27272
v  Velocity[x]            0.29288          2.1831         0.90806         0.90983
v  Velocity[y]           -0.36685         0.70427      0.00057501         0.00035
v  Velocity[z]            -0.4224         0.50576       -0.001243      -0.0013624
v  TurbEner             0.0010421        0.014935       0.0032883       0.0033471
v  Dissip              9.2053e-05        0.028188      0.00045055      0.00038965
v  TurbVisc                 0.169          11.346          4.7158          5.2766
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              227:        0.97622E-01

===============================================================


 INSTANT    0.228000000E+03   TIME STEP NUMBER             228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001134E+04
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 :  0.23752E+00 0.13252E+01
   Friction velocity        uet   :  0.14205E-01 0.78994E-01
   Friction velocity        uk    :  0.17681E-01 0.38565E-01
   Dimensionless distance   yplus :  0.43379E+03 0.95269E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72228E+01      69   0.17100E-02   0.23713E-01 
c  VelocityX    0.46302E+04      13   0.67915E-02   0.43386E-03 
c  VelocityY    0.46302E+04      13   0.67915E-02   0.58415E-04 
c  VelocityZ    0.46302E+04      13   0.67915E-02   0.48293E-04 
c  TurbEner     0.59798E+01      13   0.12682E-03   0.18492E-08 
c  Dissip       0.14035E+01      16   0.20307E-02   0.50367E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.03           54515           26779           27274
v  Velocity[x]            0.29307          2.0046         0.90807         0.90985
v  Velocity[y]           -0.38288         0.69232      0.00056271      0.00034289
v  Velocity[z]           -0.42107         0.51048      -0.0012512      -0.0013701
v  TurbEner             0.0010424        0.015587       0.0032887       0.0033473
v  Dissip              9.2087e-05        0.029777      0.00045094      0.00038993
v  TurbVisc                0.1702          11.341          4.7159          5.2768
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              228:        0.10070E+00

===============================================================


 INSTANT    0.229000000E+03   TIME STEP NUMBER             229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999211E+04
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 :  0.23798E+00 0.12280E+01
   Friction velocity        uet   :  0.14233E-01 0.72582E-01
   Friction velocity        uk    :  0.17684E-01 0.38600E-01
   Dimensionless distance   yplus :  0.43415E+03 0.95305E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60956E+01      57   0.11732E-02   0.19989E-01 
c  VelocityX    0.46304E+04      12   0.66619E-02   0.36685E-03 
c  VelocityY    0.46304E+04      12   0.66619E-02   0.34078E-04 
c  VelocityZ    0.46304E+04      12   0.66619E-02   0.35156E-04 
c  TurbEner     0.59779E+01      14   0.13330E-03   0.24875E-08 
c  Dissip       0.13815E+01      16   0.18359E-02   0.50195E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.09           54520           26778           27273
v  Velocity[x]            0.29273          2.1001         0.90805         0.90982
v  Velocity[y]           -0.36744         0.70124      0.00056468      0.00034154
v  Velocity[z]           -0.42241          0.5043      -0.0012484      -0.0013692
v  TurbEner             0.0010488        0.014926       0.0032885       0.0033472
v  Dissip              9.2124e-05        0.028541      0.00045087      0.00038987
v  TurbVisc               0.17041          11.319           4.716          5.2769
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              229:        0.96296E-01

===============================================================


 INSTANT    0.230000000E+03   TIME STEP NUMBER             230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001398E+04
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 :  0.23767E+00 0.13244E+01
   Friction velocity        uet   :  0.14215E-01 0.78948E-01
   Friction velocity        uk    :  0.17738E-01 0.38691E-01
   Dimensionless distance   yplus :  0.43468E+03 0.95339E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58920E+01      53   0.11867E-02   0.19322E-01 
c  VelocityX    0.46304E+04      12   0.70783E-02   0.28258E-03 
c  VelocityY    0.46304E+04      12   0.70783E-02   0.32933E-04 
c  VelocityZ    0.46304E+04      12   0.70783E-02   0.42529E-04 
c  TurbEner     0.59783E+01      13   0.64051E-04   0.64785E-09 
c  Dissip       0.13927E+01      14   0.30741E-03   0.25173E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.4           54535           26779           27273
v  Velocity[x]             0.2928          2.1395         0.90805         0.90983
v  Velocity[y]           -0.38221         0.69484      0.00055671      0.00033367
v  Velocity[z]           -0.41901          0.5119       -0.001257      -0.0013785
v  TurbEner             0.0010526        0.014916       0.0032886       0.0033473
v  Dissip              9.2136e-05        0.028645      0.00045096      0.00038994
v  TurbVisc               0.17082          11.323           4.716          5.2768
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              230:        0.95133E-01

===============================================================


 INSTANT    0.231000000E+03   TIME STEP NUMBER             231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000471E+04
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 :  0.23764E+00 0.12460E+01
   Friction velocity        uet   :  0.14213E-01 0.72641E-01
   Friction velocity        uk    :  0.17770E-01 0.38741E-01
   Dimensionless distance   yplus :  0.43592E+03 0.95309E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65573E+01      61   0.13791E-02   0.21502E-01 
c  VelocityX    0.46304E+04      12   0.69757E-02   0.31186E-03 
c  VelocityY    0.46304E+04      12   0.69757E-02   0.38365E-04 
c  VelocityZ    0.46304E+04      12   0.69757E-02   0.90453E-04 
c  TurbEner     0.59795E+01      13   0.70920E-04   0.87684E-09 
c  Dissip       0.14248E+01      16   0.10200E-02   0.21026E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.69           54545           26778           27272
v  Velocity[x]            0.29274          2.1771         0.90805         0.90983
v  Velocity[y]           -0.36606         0.70194      0.00056717      0.00034284
v  Velocity[z]           -0.42115         0.50649      -0.0012518      -0.0013728
v  TurbEner             0.0010522        0.015106       0.0032886       0.0033473
v  Dissip              9.2096e-05        0.029234      0.00045126      0.00039015
v  TurbVisc               0.17154          11.364           4.716          5.2769
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              231:        0.96845E-01

===============================================================


 INSTANT    0.232000000E+03   TIME STEP NUMBER             232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001556E+04
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 :  0.23768E+00 0.13261E+01
   Friction velocity        uet   :  0.14215E-01 0.79040E-01
   Friction velocity        uk    :  0.17767E-01 0.38751E-01
   Dimensionless distance   yplus :  0.43627E+03 0.95331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64833E+01      59   0.15365E-02   0.21258E-01 
c  VelocityX    0.46303E+04      12   0.70129E-02   0.46894E-03 
c  VelocityY    0.46303E+04      12   0.70129E-02   0.33699E-04 
c  VelocityZ    0.46303E+04      12   0.70129E-02   0.53864E-04 
c  TurbEner     0.59800E+01      13   0.11285E-03   0.14171E-08 
c  Dissip       0.14406E+01      16   0.19403E-02   0.47988E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.81           54552           26779           27273
v  Velocity[x]            0.29269          2.0151         0.90808         0.90986
v  Velocity[y]           -0.38222         0.69571      0.00055376      0.00033197
v  Velocity[z]           -0.42338         0.51121      -0.0012667      -0.0013877
v  TurbEner             0.0010548         0.01564        0.003289       0.0033476
v  Dissip              9.2104e-05        0.030731      0.00045163      0.00039041
v  TurbVisc               0.17161          11.352           4.716          5.2769
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              232:        0.96609E-01

===============================================================


 INSTANT    0.233000000E+03   TIME STEP NUMBER             233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997593E+04
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 :  0.23783E+00 0.12144E+01
   Friction velocity        uet   :  0.14224E-01 0.72388E-01
   Friction velocity        uk    :  0.17789E-01 0.38744E-01
   Dimensionless distance   yplus :  0.43600E+03 0.95337E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60954E+01      55   0.15654E-02   0.19984E-01 
c  VelocityX    0.46303E+04      13   0.66015E-02   0.37617E-03 
c  VelocityY    0.46303E+04      13   0.66015E-02   0.27109E-04 
c  VelocityZ    0.46303E+04      13   0.66015E-02   0.37774E-04 
c  TurbEner     0.59790E+01      14   0.13866E-03   0.22145E-08 
c  Dissip       0.14161E+01      16   0.18381E-02   0.54608E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.83           54544           26778           27272
v  Velocity[x]            0.29312          2.0925         0.90806         0.90984
v  Velocity[y]           -0.36765         0.70428      0.00056425      0.00034117
v  Velocity[z]           -0.41975         0.50426       -0.001254      -0.0013737
v  TurbEner             0.0010575        0.015041        0.003289       0.0033476
v  Dissip              9.2127e-05        0.029578      0.00045157      0.00039038
v  TurbVisc               0.17146           11.35          4.7161           5.277
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              233:        0.96653E-01

===============================================================


 INSTANT    0.234000000E+03   TIME STEP NUMBER             234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000622E+04
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 :  0.23779E+00 0.13257E+01
   Friction velocity        uet   :  0.14222E-01 0.79020E-01
   Friction velocity        uk    :  0.17812E-01 0.38761E-01
   Dimensionless distance   yplus :  0.43717E+03 0.95299E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66903E+01      59   0.15814E-02   0.21947E-01 
c  VelocityX    0.46303E+04      13   0.68036E-02   0.32571E-03 
c  VelocityY    0.46303E+04      13   0.68036E-02   0.39126E-04 
c  VelocityZ    0.46303E+04      13   0.68036E-02   0.43246E-04 
c  TurbEner     0.59797E+01      13   0.74911E-04   0.10600E-08 
c  Dissip       0.14253E+01      14   0.36801E-03   0.37654E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.19           54522           26779           27273
v  Velocity[x]            0.29279          2.1338         0.90809         0.90987
v  Velocity[y]           -0.38243         0.69217       0.0005537      0.00033541
v  Velocity[z]            -0.4214         0.51175      -0.0012583      -0.0013767
v  TurbEner             0.0010532        0.014961       0.0032892       0.0033479
v  Dissip              9.2123e-05        0.029514      0.00045173       0.0003905
v  TurbVisc               0.17206          11.382          4.7161          5.2771
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              234:        0.96810E-01

===============================================================


 INSTANT    0.235000000E+03   TIME STEP NUMBER             235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999161E+04
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 :  0.23784E+00 0.12365E+01
   Friction velocity        uet   :  0.14225E-01 0.72618E-01
   Friction velocity        uk    :  0.17775E-01 0.38709E-01
   Dimensionless distance   yplus :  0.43673E+03 0.95349E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73564E+01      62   0.14201E-02   0.24119E-01 
c  VelocityX    0.46303E+04      12   0.73580E-02   0.37321E-03 
c  VelocityY    0.46303E+04      12   0.73580E-02   0.55133E-04 
c  VelocityZ    0.46303E+04      12   0.73580E-02   0.90517E-04 
c  TurbEner     0.59803E+01      13   0.65911E-04   0.10388E-08 
c  Dissip       0.14554E+01      15   0.89291E-03   0.18162E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.16           54530           26778           27272
v  Velocity[x]             0.2928          2.1815         0.90804         0.90982
v  Velocity[y]           -0.36656         0.70086      0.00056519      0.00034221
v  Velocity[z]           -0.42282         0.50611      -0.0012541      -0.0013766
v  TurbEner             0.0010551        0.015062       0.0032893       0.0033479
v  Dissip              9.2076e-05        0.029924      0.00045199      0.00039067
v  TurbVisc               0.17165          11.359          4.7162          5.2772
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              235:        0.96594E-01

===============================================================


 INSTANT    0.236000000E+03   TIME STEP NUMBER             236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001297E+04
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 :  0.23786E+00 0.13241E+01
   Friction velocity        uet   :  0.14226E-01 0.78922E-01
   Friction velocity        uk    :  0.17791E-01 0.38738E-01
   Dimensionless distance   yplus :  0.43641E+03 0.95401E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64552E+01      57   0.14153E-02   0.21174E-01 
c  VelocityX    0.46302E+04      12   0.65850E-02   0.43908E-03 
c  VelocityY    0.46302E+04      12   0.65850E-02   0.31923E-04 
c  VelocityZ    0.46302E+04      12   0.65850E-02   0.46340E-04 
c  TurbEner     0.59804E+01      13   0.11981E-03   0.14311E-08 
c  Dissip       0.14687E+01      16   0.19811E-02   0.45876E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -171.3           54539           26778           27272
v  Velocity[x]            0.29277          2.0087         0.90806         0.90984
v  Velocity[y]           -0.38221         0.69505      0.00055207      0.00032891
v  Velocity[z]           -0.42105         0.51114      -0.0012555      -0.0013755
v  TurbEner             0.0010543        0.015658       0.0032894        0.003348
v  Dissip              9.2096e-05        0.031481      0.00045226      0.00039088
v  TurbVisc               0.17147          11.354          4.7162          5.2772
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              236:        0.96013E-01

===============================================================


 INSTANT    0.237000000E+03   TIME STEP NUMBER             237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999455E+04
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 :  0.23791E+00 0.12174E+01
   Friction velocity        uet   :  0.14230E-01 0.72575E-01
   Friction velocity        uk    :  0.17784E-01 0.38708E-01
   Dimensionless distance   yplus :  0.43670E+03 0.95348E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58597E+01      55   0.11975E-02   0.19216E-01 
c  VelocityX    0.46302E+04      13   0.63326E-02   0.36799E-03 
c  VelocityY    0.46302E+04      13   0.63326E-02   0.23395E-04 
c  VelocityZ    0.46302E+04      13   0.63326E-02   0.34638E-04 
c  TurbEner     0.59790E+01      13   0.14728E-03   0.20480E-08 
c  Dissip       0.14347E+01      17   0.22873E-02   0.69904E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.08           54545           26777           27272
v  Velocity[x]            0.29287          2.0951         0.90806         0.90984
v  Velocity[y]           -0.36701         0.70336      0.00054708       0.0003245
v  Velocity[z]           -0.42226         0.50473      -0.0012597      -0.0013813
v  TurbEner              0.001051        0.014917       0.0032892       0.0033479
v  Dissip              9.2087e-05         0.02989      0.00045214       0.0003908
v  TurbVisc               0.17159          11.327          4.7162          5.2771
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              237:        0.95293E-01

===============================================================


 INSTANT    0.238000000E+03   TIME STEP NUMBER             238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001899E+04
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 :  0.23766E+00 0.13243E+01
   Friction velocity        uet   :  0.14216E-01 0.78940E-01
   Friction velocity        uk    :  0.17757E-01 0.38765E-01
   Dimensionless distance   yplus :  0.43645E+03 0.95329E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63932E+01      52   0.12436E-02   0.20966E-01 
c  VelocityX    0.46302E+04      12   0.65382E-02   0.32899E-03 
c  VelocityY    0.46302E+04      12   0.65382E-02   0.36399E-04 
c  VelocityZ    0.46302E+04      12   0.65382E-02   0.35805E-04 
c  TurbEner     0.59792E+01      12   0.60828E-04   0.64913E-09 
c  Dissip       0.14353E+01      13   0.36455E-03   0.21240E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.71           54553           26777           27272
v  Velocity[x]             0.2929          2.1328         0.90808         0.90986
v  Velocity[y]           -0.38241         0.69594      0.00054414      0.00032433
v  Velocity[z]            -0.4228         0.51178      -0.0012607      -0.0013804
v  TurbEner             0.0010516        0.014827       0.0032892        0.003348
v  Dissip              9.2099e-05        0.029661      0.00045216      0.00039082
v  TurbVisc                0.1713          11.338          4.7161          5.2771
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              238:        0.95222E-01

===============================================================


 INSTANT    0.239000000E+03   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001107E+04
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 :  0.23773E+00 0.12300E+01
   Friction velocity        uet   :  0.14221E-01 0.72578E-01
   Friction velocity        uk    :  0.17761E-01 0.38798E-01
   Dimensionless distance   yplus :  0.43574E+03 0.95303E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64863E+01      58   0.15575E-02   0.21255E-01 
c  VelocityX    0.46302E+04      12   0.78316E-02   0.31725E-03 
c  VelocityY    0.46302E+04      12   0.78316E-02   0.38203E-04 
c  VelocityZ    0.46302E+04      12   0.78316E-02   0.62561E-04 
c  TurbEner     0.59806E+01      12   0.69650E-04   0.77008E-09 
c  Dissip       0.14572E+01      15   0.79662E-03   0.12294E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.88           54542           26777           27271
v  Velocity[x]            0.29279          2.1705         0.90805         0.90983
v  Velocity[y]           -0.36688         0.70197      0.00056067      0.00033612
v  Velocity[z]           -0.42021         0.50568      -0.0012572      -0.0013796
v  TurbEner             0.0010532        0.015023       0.0032894       0.0033481
v  Dissip              9.2076e-05        0.030119      0.00045232      0.00039093
v  TurbVisc               0.17088          11.305          4.7161           5.277
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              239:        0.96291E-01

===============================================================


 INSTANT    0.240000000E+03   TIME STEP NUMBER             240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001330E+04
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 :  0.23730E+00 0.13259E+01
   Friction velocity        uet   :  0.14195E-01 0.79031E-01
   Friction velocity        uk    :  0.17775E-01 0.38818E-01
   Dimensionless distance   yplus :  0.43663E+03 0.95251E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63209E+01      64   0.15591E-02   0.20736E-01 
c  VelocityX    0.46302E+04      13   0.77777E-02   0.36713E-03 
c  VelocityY    0.46302E+04      13   0.77777E-02   0.27218E-04 
c  VelocityZ    0.46302E+04      13   0.77777E-02   0.47100E-04 
c  TurbEner     0.59817E+01      13   0.83767E-04   0.14148E-08 
c  Dissip       0.14869E+01      15   0.10256E-02   0.21655E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.61           54518           26778           27272
v  Velocity[x]            0.29255          2.1942         0.90808         0.90986
v  Velocity[y]           -0.38286         0.69537      0.00055401      0.00033629
v  Velocity[z]            -0.4204         0.51052      -0.0012513      -0.0013732
v  TurbEner             0.0010483         0.01524       0.0032895       0.0033482
v  Dissip              9.2081e-05        0.030706      0.00045259      0.00039112
v  TurbVisc               0.17129          11.304          4.7161           5.277
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              240:        0.97645E-01

===============================================================


 INSTANT    0.241000000E+03   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998298E+04
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 :  0.23772E+00 0.12614E+01
   Friction velocity        uet   :  0.14220E-01 0.73662E-01
   Friction velocity        uk    :  0.17734E-01 0.38723E-01
   Dimensionless distance   yplus :  0.43596E+03 0.95258E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70458E+01      60   0.16056E-02   0.23094E-01 
c  VelocityX    0.46301E+04      13   0.69001E-02   0.47981E-03 
c  VelocityY    0.46301E+04      13   0.69001E-02   0.44496E-04 
c  VelocityZ    0.46301E+04      13   0.69001E-02   0.88494E-04 
c  TurbEner     0.59819E+01      13   0.12343E-03   0.17809E-08 
c  Dissip       0.15079E+01      16   0.21018E-02   0.52832E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.44           54524           26777           27271
v  Velocity[x]            0.29295          2.0368         0.90805         0.90982
v  Velocity[y]           -0.36741         0.70309      0.00055729      0.00033243
v  Velocity[z]           -0.42132         0.50432      -0.0012565      -0.0013783
v  TurbEner             0.0010501        0.015836       0.0032897       0.0033483
v  Dissip              9.2032e-05        0.032385      0.00045292      0.00039136
v  TurbVisc                0.1707           11.33          4.7159          5.2769
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              241:        0.97120E-01

===============================================================


 INSTANT    0.242000000E+03   TIME STEP NUMBER             242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001778E+04
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 :  0.23811E+00 0.13255E+01
   Friction velocity        uet   :  0.14243E-01 0.79015E-01
   Friction velocity        uk    :  0.17749E-01 0.38726E-01
   Dimensionless distance   yplus :  0.43550E+03 0.95235E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61741E+01      58   0.12279E-02   0.20241E-01 
c  VelocityX    0.46300E+04      12   0.66570E-02   0.37121E-03 
c  VelocityY    0.46300E+04      12   0.66570E-02   0.30253E-04 
c  VelocityZ    0.46300E+04      12   0.66570E-02   0.44839E-04 
c  TurbEner     0.59805E+01      13   0.12634E-03   0.17718E-08 
c  Dissip       0.14823E+01      16   0.17299E-02   0.48415E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.19           54534           26777           27271
v  Velocity[x]            0.29283          2.1016         0.90806         0.90984
v  Velocity[y]           -0.38223         0.69254      0.00054895      0.00032753
v  Velocity[z]           -0.42179         0.51183      -0.0012495      -0.0013699
v  TurbEner             0.0010495        0.015301       0.0032895       0.0033482
v  Dissip              9.2048e-05        0.031271      0.00045281       0.0003913
v  TurbVisc               0.17036          11.317          4.7158          5.2768
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              242:        0.96302E-01

===============================================================


 INSTANT    0.243000000E+03   TIME STEP NUMBER             243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998423E+04
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 :  0.23769E+00 0.12178E+01
   Friction velocity        uet   :  0.14218E-01 0.72595E-01
   Friction velocity        uk    :  0.17744E-01 0.38750E-01
   Dimensionless distance   yplus :  0.43583E+03 0.95184E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61382E+01      52   0.12249E-02   0.20127E-01 
c  VelocityX    0.46301E+04      12   0.69073E-02   0.31908E-03 
c  VelocityY    0.46301E+04      12   0.69073E-02   0.26111E-04 
c  VelocityZ    0.46301E+04      12   0.69073E-02   0.33103E-04 
c  TurbEner     0.59807E+01      12   0.65992E-04   0.63229E-09 
c  Dissip       0.14928E+01      13   0.35979E-03   0.29484E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.89           54541           26777           27271
v  Velocity[x]            0.29253          2.1602         0.90807         0.90984
v  Velocity[y]           -0.36606         0.69994      0.00054355      0.00032125
v  Velocity[z]           -0.42241         0.50655      -0.0012575       -0.001379
v  TurbEner             0.0010455        0.015166       0.0032894       0.0033481
v  Dissip               9.205e-05        0.031154       0.0004529      0.00039136
v  TurbVisc               0.17041          11.324          4.7157          5.2766
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              243:        0.95177E-01

===============================================================


 INSTANT    0.244000000E+03   TIME STEP NUMBER             244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001155E+04
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 :  0.23771E+00 0.13237E+01
   Friction velocity        uet   :  0.14220E-01 0.78904E-01
   Friction velocity        uk    :  0.17710E-01 0.38786E-01
   Dimensionless distance   yplus :  0.43539E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61786E+01      52   0.11800E-02   0.20259E-01 
c  VelocityX    0.46301E+04      12   0.70196E-02   0.30766E-03 
c  VelocityY    0.46301E+04      12   0.70196E-02   0.29816E-04 
c  VelocityZ    0.46301E+04      12   0.70196E-02   0.33705E-04 
c  TurbEner     0.59814E+01      12   0.63964E-04   0.73387E-09 
c  Dissip       0.15166E+01      15   0.86537E-03   0.16462E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.82           54551           26777           27272
v  Velocity[x]            0.29281          2.1763         0.90807         0.90985
v  Velocity[y]           -0.38227         0.69334      0.00054085      0.00032181
v  Velocity[z]           -0.42207          0.5111      -0.0012576      -0.0013769
v  TurbEner             0.0010449        0.015283       0.0032894       0.0033481
v  Dissip              9.2049e-05        0.031589       0.0004531      0.00039149
v  TurbVisc               0.16994          11.362          4.7155          5.2764
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              244:        0.95389E-01

===============================================================


 INSTANT    0.245000000E+03   TIME STEP NUMBER             245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998097E+04
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 :  0.23794E+00 0.12370E+01
   Friction velocity        uet   :  0.14233E-01 0.72485E-01
   Friction velocity        uk    :  0.17705E-01 0.38772E-01
   Dimensionless distance   yplus :  0.43440E+03 0.95250E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66283E+01      56   0.15680E-02   0.21736E-01 
c  VelocityX    0.46300E+04      13   0.78298E-02   0.36924E-03 
c  VelocityY    0.46300E+04      13   0.78298E-02   0.43560E-04 
c  VelocityZ    0.46300E+04      13   0.78298E-02   0.65753E-04 
c  TurbEner     0.59821E+01      13   0.11835E-03   0.11501E-08 
c  Dissip       0.15374E+01      16   0.21377E-02   0.52029E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.98           54542           26777           27271
v  Velocity[x]              0.293          2.0196         0.90805         0.90982
v  Velocity[y]           -0.36772         0.70207       0.0005591      0.00033571
v  Velocity[z]           -0.41995          0.5042      -0.0012564      -0.0013755
v  TurbEner             0.0010454        0.015871       0.0032895       0.0033482
v  Dissip              9.2049e-05        0.033309      0.00045337      0.00039169
v  TurbVisc               0.16932          11.348          4.7153          5.2762
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              245:        0.96418E-01

===============================================================


 INSTANT    0.246000000E+03   TIME STEP NUMBER             246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000833E+04
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 :  0.23723E+00 0.13241E+01
   Friction velocity        uet   :  0.14190E-01 0.78930E-01
   Friction velocity        uk    :  0.17710E-01 0.38743E-01
   Dimensionless distance   yplus :  0.43504E+03 0.95247E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64384E+01      63   0.16415E-02   0.21122E-01 
c  VelocityX    0.46300E+04      12   0.67954E-02   0.40165E-03 
c  VelocityY    0.46300E+04      12   0.67954E-02   0.32588E-04 
c  VelocityZ    0.46300E+04      12   0.67954E-02   0.43757E-04 
c  TurbEner     0.59806E+01      14   0.15695E-03   0.24221E-08 
c  Dissip       0.15035E+01      16   0.21999E-02   0.65587E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.66           54517           26778           27272
v  Velocity[x]             0.2926          2.0939         0.90808         0.90985
v  Velocity[y]           -0.38253         0.69437      0.00054867      0.00033136
v  Velocity[z]           -0.42014         0.51176      -0.0012478       -0.001368
v  TurbEner             0.0010395        0.015154       0.0032893       0.0033481
v  Dissip              9.2006e-05         0.03177      0.00045322       0.0003916
v  TurbVisc               0.16958          11.352          4.7152          5.2761
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              246:        0.97084E-01

===============================================================


 INSTANT    0.247000000E+03   TIME STEP NUMBER             247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999375E+04
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 :  0.23788E+00 0.12647E+01
   Friction velocity        uet   :  0.14229E-01 0.73722E-01
   Friction velocity        uk    :  0.17659E-01 0.38661E-01
   Dimensionless distance   yplus :  0.43416E+03 0.95294E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60673E+01      59   0.12635E-02   0.19888E-01 
c  VelocityX    0.46301E+04      12   0.70042E-02   0.40177E-03 
c  VelocityY    0.46301E+04      12   0.70042E-02   0.25186E-04 
c  VelocityZ    0.46301E+04      12   0.70042E-02   0.37420E-04 
c  TurbEner     0.59799E+01      13   0.70096E-04   0.10038E-08 
c  Dissip       0.15113E+01      13   0.45613E-03   0.31473E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.9           54522           26777           27271
v  Velocity[x]            0.29274          2.1545         0.90806         0.90982
v  Velocity[y]           -0.36653         0.70072       0.0005519      0.00032974
v  Velocity[z]           -0.42128         0.50599      -0.0012501        -0.00137
v  TurbEner             0.0010405        0.014974       0.0032891       0.0033479
v  Dissip              9.2052e-05        0.031469       0.0004532      0.00039159
v  TurbVisc               0.16891          11.328          4.7149          5.2759
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              247:        0.96238E-01

===============================================================


 INSTANT    0.248000000E+03   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002589E+04
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 :  0.23789E+00 0.13256E+01
   Friction velocity        uet   :  0.14229E-01 0.79015E-01
   Friction velocity        uk    :  0.17668E-01 0.38672E-01
   Dimensionless distance   yplus :  0.43353E+03 0.95325E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71448E+01      55   0.14719E-02   0.23415E-01 
c  VelocityX    0.46299E+04      12   0.75810E-02   0.36878E-03 
c  VelocityY    0.46299E+04      12   0.75810E-02   0.32701E-04 
c  VelocityZ    0.46299E+04      12   0.75810E-02   0.96750E-04 
c  TurbEner     0.59805E+01      13   0.75339E-04   0.97549E-09 
c  Dissip       0.15314E+01      15   0.69815E-03   0.12255E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.7           54528           26777           27271
v  Velocity[x]            0.29301           2.188         0.90806         0.90984
v  Velocity[y]           -0.38223         0.69411      0.00055839      0.00033851
v  Velocity[z]           -0.42191         0.51105      -0.0012419      -0.0013644
v  TurbEner             0.0010396        0.015061        0.003289       0.0033478
v  Dissip              9.2091e-05        0.031654      0.00045331      0.00039165
v  TurbVisc               0.16854          11.322          4.7147          5.2756
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              248:        0.95377E-01

===============================================================


 INSTANT    0.249000000E+03   TIME STEP NUMBER             249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000324E+04
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 :  0.23753E+00 0.12287E+01
   Friction velocity        uet   :  0.14207E-01 0.72312E-01
   Friction velocity        uk    :  0.17660E-01 0.38740E-01
   Dimensionless distance   yplus :  0.43380E+03 0.95313E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63556E+01      53   0.14840E-02   0.20847E-01 
c  VelocityX    0.46299E+04      13   0.67380E-02   0.41992E-03 
c  VelocityY    0.46299E+04      13   0.67380E-02   0.44191E-04 
c  VelocityZ    0.46299E+04      13   0.67380E-02   0.65969E-04 
c  TurbEner     0.59806E+01      13   0.12498E-03   0.12463E-08 
c  Dissip       0.15411E+01      16   0.20089E-02   0.43385E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.09           54517           26776           27271
v  Velocity[x]            0.29256          2.0172         0.90807         0.90983
v  Velocity[y]           -0.36696         0.70302      0.00056255      0.00033912
v  Velocity[z]           -0.42196          0.5047      -0.0012511      -0.0013716
v  TurbEner             0.0010354        0.015667       0.0032889       0.0033477
v  Dissip               9.211e-05        0.033256      0.00045349      0.00039179
v  TurbVisc               0.16864          11.348          4.7145          5.2755
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              249:        0.96146E-01

===============================================================


 INSTANT    0.250000000E+03   TIME STEP NUMBER             250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999813E+04
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 :  0.23784E+00 0.13247E+01
   Friction velocity        uet   :  0.14225E-01 0.78965E-01
   Friction velocity        uk    :  0.17625E-01 0.38759E-01
   Dimensionless distance   yplus :  0.43334E+03 0.95359E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        250, Physical time    0.25000E+03


   ** 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:    0.74411E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61783E+01      54   0.12111E-02   0.20253E-01 
c  VelocityX    0.46299E+04      12   0.72099E-02   0.41737E-03 
c  VelocityY    0.46299E+04      12   0.72099E-02   0.36527E-04 
c  VelocityZ    0.46299E+04      12   0.72099E-02   0.43525E-04 
c  TurbEner     0.59786E+01      14   0.15628E-03   0.25548E-08 
c  Dissip       0.15004E+01      17   0.24903E-02   0.84704E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.12           54516           26777           27271
v  Velocity[x]            0.29265          2.1032         0.90805         0.90983
v  Velocity[y]           -0.38242         0.69422      0.00055615      0.00033513
v  Velocity[z]           -0.42186         0.51168      -0.0012528      -0.0013739
v  TurbEner              0.001035        0.014929       0.0032885       0.0033474
v  Dissip              9.2095e-05        0.031558      0.00045316      0.00039155
v  TurbVisc               0.16823          11.331          4.7143          5.2753
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              250:        0.10325E+00

===============================================================


 INSTANT    0.251000000E+03   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998347E+04
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 :  0.23783E+00 0.12192E+01
   Friction velocity        uet   :  0.14225E-01 0.72490E-01
   Friction velocity        uk    :  0.17621E-01 0.38758E-01
   Dimensionless distance   yplus :  0.43243E+03 0.95337E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59632E+01      54   0.12976E-02   0.19545E-01 
c  VelocityX    0.46299E+04      12   0.70251E-02   0.36741E-03 
c  VelocityY    0.46299E+04      12   0.70251E-02   0.26561E-04 
c  VelocityZ    0.46299E+04      12   0.70251E-02   0.32172E-04 
c  TurbEner     0.59783E+01      13   0.69400E-04   0.81881E-09 
c  Dissip       0.15067E+01      13   0.36559E-03   0.24585E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.71           54530           26776           27270
v  Velocity[x]            0.29325          2.1499         0.90806         0.90984
v  Velocity[y]           -0.36686         0.70037      0.00055878      0.00033414
v  Velocity[z]           -0.41989         0.50569      -0.0012587      -0.0013775
v  TurbEner             0.0010357        0.014808        0.003288       0.0033471
v  Dissip              9.2115e-05        0.031372      0.00045299      0.00039143
v  TurbVisc               0.16772           11.32          4.7141          5.2751
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              251:        0.95820E-01

===============================================================


 INSTANT    0.252000000E+03   TIME STEP NUMBER             252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001462E+04
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 :  0.23749E+00 0.13253E+01
   Friction velocity        uet   :  0.14204E-01 0.78997E-01
   Friction velocity        uk    :  0.17627E-01 0.38686E-01
   Dimensionless distance   yplus :  0.43313E+03 0.95341E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57292E+01      53   0.14263E-02   0.18787E-01 
c  VelocityX    0.46300E+04      12   0.68090E-02   0.29860E-03 
c  VelocityY    0.46300E+04      12   0.68090E-02   0.34404E-04 
c  VelocityZ    0.46300E+04      12   0.68090E-02   0.60668E-04 
c  TurbEner     0.59791E+01      12   0.82641E-04   0.93924E-09 
c  Dissip       0.15299E+01      15   0.83787E-03   0.14912E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.77           54541           26776           27270
v  Velocity[x]            0.29282          2.1843         0.90805         0.90983
v  Velocity[y]           -0.38288         0.69205      0.00055922      0.00033675
v  Velocity[z]           -0.42041         0.51042      -0.0012485      -0.0013726
v  TurbEner               0.00103        0.014931       0.0032879       0.0033469
v  Dissip              9.2101e-05        0.031776      0.00045308      0.00039148
v  TurbVisc               0.16806           11.36          4.7138          5.2748
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              252:        0.95045E-01

===============================================================


 INSTANT    0.253000000E+03   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001078E+04
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 :  0.23795E+00 0.12151E+01
   Friction velocity        uet   :  0.14232E-01 0.72432E-01
   Friction velocity        uk    :  0.17578E-01 0.38666E-01
   Dimensionless distance   yplus :  0.43230E+03 0.95317E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65825E+01      57   0.13076E-02   0.21581E-01 
c  VelocityX    0.46299E+04      12   0.72861E-02   0.30580E-03 
c  VelocityY    0.46299E+04      12   0.72861E-02   0.52479E-04 
c  VelocityZ    0.46299E+04      12   0.72861E-02   0.50360E-04 
c  TurbEner     0.59796E+01      13   0.78020E-04   0.10394E-08 
c  Dissip       0.15583E+01      15   0.10226E-02   0.21655E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.16           54548           26776           27270
v  Velocity[x]            0.29248          2.2004         0.90806         0.90983
v  Velocity[y]           -0.36745         0.70068      0.00055552      0.00033359
v  Velocity[z]           -0.42291         0.50426      -0.0012592        -0.00138
v  TurbEner             0.0010309        0.015124       0.0032877       0.0033468
v  Dissip              9.2134e-05        0.032332      0.00045321      0.00039156
v  TurbVisc               0.16746          11.344          4.7137          5.2747
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              253:        0.95765E-01

===============================================================


 INSTANT    0.254000000E+03   TIME STEP NUMBER             254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000679E+04
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 :  0.23763E+00 0.13228E+01
   Friction velocity        uet   :  0.14212E-01 0.78857E-01
   Friction velocity        uk    :  0.17586E-01 0.38748E-01
   Dimensionless distance   yplus :  0.43168E+03 0.95262E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.81784E+01      58   0.18141E-02   0.26804E-01 
c  VelocityX    0.46298E+04      12   0.73590E-02   0.39344E-03 
c  VelocityY    0.46298E+04      12   0.73590E-02   0.46163E-04 
c  VelocityZ    0.46298E+04      12   0.73590E-02   0.92375E-04 
c  TurbEner     0.59803E+01      13   0.12239E-03   0.13395E-08 
c  Dissip       0.15827E+01      16   0.22079E-02   0.56398E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.93           54541           26776           27270
v  Velocity[x]            0.29276          2.0495         0.90804         0.90982
v  Velocity[y]           -0.38234         0.69361      0.00056686      0.00034586
v  Velocity[z]           -0.41951         0.51181      -0.0012397      -0.0013631
v  TurbEner             0.0010293        0.015701       0.0032875       0.0033467
v  Dissip              9.2129e-05         0.03409      0.00045341      0.00039171
v  TurbVisc               0.16712          11.346          4.7134          5.2745
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              254:        0.95824E-01

===============================================================


 INSTANT    0.255000000E+03   TIME STEP NUMBER             255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999129E+04
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 :  0.23765E+00 0.12175E+01
   Friction velocity        uet   :  0.14213E-01 0.72487E-01
   Friction velocity        uk    :  0.17573E-01 0.38779E-01
   Dimensionless distance   yplus :  0.43178E+03 0.95286E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71931E+01      64   0.17112E-02   0.23602E-01 
c  VelocityX    0.46298E+04      12   0.66790E-02   0.40480E-03 
c  VelocityY    0.46298E+04      12   0.66790E-02   0.38997E-04 
c  VelocityZ    0.46298E+04      12   0.66790E-02   0.53248E-04 
c  TurbEner     0.59789E+01      13   0.12871E-03   0.19344E-08 
c  Dissip       0.15546E+01      16   0.18294E-02   0.53623E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.91           54518           26776           27270
v  Velocity[x]            0.29289          2.1045         0.90805         0.90982
v  Velocity[y]           -0.36613         0.70034      0.00056488       0.0003466
v  Velocity[z]            -0.4211         0.50647      -0.0012455      -0.0013667
v  TurbEner             0.0010251        0.015207       0.0032872       0.0033464
v  Dissip              9.2114e-05        0.032925       0.0004532      0.00039158
v  TurbVisc               0.16715          11.322          4.7132          5.2743
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              255:        0.96857E-01

===============================================================


 INSTANT    0.256000000E+03   TIME STEP NUMBER             256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000304E+04
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 :  0.23776E+00 0.13247E+01
   Friction velocity        uet   :  0.14220E-01 0.78965E-01
   Friction velocity        uk    :  0.17536E-01 0.38780E-01
   Dimensionless distance   yplus :  0.43130E+03 0.95301E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60193E+01      57   0.11888E-02   0.19730E-01 
c  VelocityX    0.46299E+04      12   0.65398E-02   0.36364E-03 
c  VelocityY    0.46299E+04      12   0.65398E-02   0.27201E-04 
c  VelocityZ    0.46299E+04      12   0.65398E-02   0.39336E-04 
c  TurbEner     0.59782E+01      13   0.72603E-04   0.10206E-08 
c  Dissip       0.15567E+01      13   0.53948E-03   0.42315E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.9           54526           26776           27270
v  Velocity[x]            0.29272          2.1656         0.90805         0.90983
v  Velocity[y]           -0.38227           0.694      0.00055903      0.00033919
v  Velocity[z]           -0.42176         0.51117      -0.0012495      -0.0013712
v  TurbEner              0.001024         0.01503        0.003287       0.0033463
v  Dissip              9.2071e-05        0.032583      0.00045319      0.00039157
v  TurbVisc               0.16675          11.328           4.713          5.2741
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              256:        0.95645E-01

===============================================================


 INSTANT    0.257000000E+03   TIME STEP NUMBER             257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000429E+04
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 :  0.23809E+00 0.12144E+01
   Friction velocity        uet   :  0.14241E-01 0.72319E-01
   Friction velocity        uk    :  0.17527E-01 0.38725E-01
   Dimensionless distance   yplus :  0.43033E+03 0.95298E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58270E+01      56   0.11424E-02   0.19101E-01 
c  VelocityX    0.46299E+04      12   0.64694E-02   0.33850E-03 
c  VelocityY    0.46299E+04      12   0.64694E-02   0.27681E-04 
c  VelocityZ    0.46299E+04      12   0.64694E-02   0.33689E-04 
c  TurbEner     0.59786E+01      13   0.66891E-04   0.79846E-09 
c  Dissip       0.15775E+01      15   0.68709E-03   0.11205E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.55           54533           26775           27269
v  Velocity[x]            0.29305           2.189         0.90806         0.90983
v  Velocity[y]            -0.3677         0.70268      0.00056016      0.00033547
v  Velocity[z]           -0.42147         0.50421      -0.0012523        -0.00137
v  TurbEner             0.0010238        0.015136       0.0032868       0.0033461
v  Dissip              9.2013e-05        0.032846      0.00045326      0.00039162
v  TurbVisc               0.16621          11.365          4.7128          5.2739
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              257:        0.96038E-01

===============================================================


 INSTANT    0.258000000E+03   TIME STEP NUMBER             258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001980E+04
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 :  0.23788E+00 0.13252E+01
   Friction velocity        uet   :  0.14228E-01 0.78999E-01
   Friction velocity        uk    :  0.17525E-01 0.38757E-01
   Dimensionless distance   yplus :  0.43083E+03 0.95361E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60754E+01      51   0.14483E-02   0.19926E-01 
c  VelocityX    0.46298E+04      12   0.69709E-02   0.32123E-03 
c  VelocityY    0.46298E+04      12   0.69709E-02   0.40164E-04 
c  VelocityZ    0.46298E+04      12   0.69709E-02   0.39670E-04 
c  TurbEner     0.59789E+01      13   0.12307E-03   0.11749E-08 
c  Dissip       0.15884E+01      16   0.20075E-02   0.44103E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.6           54541           26775           27269
v  Velocity[x]            0.29251          2.0202         0.90805         0.90983
v  Velocity[y]           -0.38239         0.69275      0.00055304      0.00033314
v  Velocity[z]           -0.42314          0.5117      -0.0012559      -0.0013777
v  TurbEner             0.0010171        0.015727       0.0032867        0.003346
v  Dissip              9.2056e-05        0.034439      0.00045347      0.00039177
v  TurbVisc               0.16644          11.347          4.7126          5.2737
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              258:        0.95024E-01

===============================================================


 INSTANT    0.259000000E+03   TIME STEP NUMBER             259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999409E+04
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 :  0.23761E+00 0.12457E+01
   Friction velocity        uet   :  0.14213E-01 0.72731E-01
   Friction velocity        uk    :  0.17468E-01 0.38729E-01
   Dimensionless distance   yplus :  0.42980E+03 0.95410E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.51367E+01      51   0.10385E-02   0.16834E-01 
c  VelocityX    0.46298E+04      12   0.65907E-02   0.30721E-03 
c  VelocityY    0.46298E+04      12   0.65907E-02   0.26098E-04 
c  VelocityZ    0.46298E+04      12   0.65907E-02   0.35867E-04 
c  TurbEner     0.59775E+01      13   0.15860E-03   0.19097E-08 
c  Dissip       0.15467E+01      16   0.25729E-02   0.89777E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.09           54548           26775           27269
v  Velocity[x]            0.29271          2.0999         0.90805         0.90982
v  Velocity[y]           -0.36657         0.70023      0.00055384      0.00033049
v  Velocity[z]           -0.42169         0.50603      -0.0012616      -0.0013817
v  TurbEner             0.0010171        0.015024       0.0032864       0.0033458
v  Dissip              9.2063e-05         0.03269      0.00045314      0.00039154
v  TurbVisc               0.16563           11.35          4.7124          5.2736
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              259:        0.94017E-01

===============================================================


 INSTANT    0.260000000E+03   TIME STEP NUMBER             260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000984E+04
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 :  0.23790E+00 0.13244E+01
   Friction velocity        uet   :  0.14231E-01 0.78946E-01
   Friction velocity        uk    :  0.17468E-01 0.38751E-01
   Dimensionless distance   yplus :  0.42900E+03 0.95363E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58355E+01      59   0.15130E-02   0.19131E-01 
c  VelocityX    0.46298E+04      12   0.73765E-02   0.35669E-03 
c  VelocityY    0.46298E+04      12   0.73765E-02   0.22029E-04 
c  VelocityZ    0.46298E+04      12   0.73765E-02   0.30936E-04 
c  TurbEner     0.59777E+01      12   0.59927E-04   0.54897E-09 
c  Dissip       0.15465E+01      13   0.54837E-03   0.36727E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.83           54540           26776           27270
v  Velocity[x]            0.29287          2.1567         0.90806         0.90984
v  Velocity[y]           -0.38227         0.69365      0.00055041      0.00033138
v  Velocity[z]           -0.42029         0.51106      -0.0012502      -0.0013705
v  TurbEner             0.0010152        0.014883       0.0032862       0.0033457
v  Dissip              9.2079e-05         0.03231      0.00045305      0.00039148
v  TurbVisc               0.16534          11.327          4.7123          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              260:        0.96227E-01

===============================================================


 INSTANT    0.261000000E+03   TIME STEP NUMBER             261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997203E+04
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 :  0.23729E+00 0.12667E+01
   Friction velocity        uet   :  0.14195E-01 0.73777E-01
   Friction velocity        uk    :  0.17452E-01 0.38781E-01
   Dimensionless distance   yplus :  0.42904E+03 0.95361E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67509E+01      56   0.17301E-02   0.22132E-01 
c  VelocityX    0.46298E+04      13   0.73056E-02   0.46776E-03 
c  VelocityY    0.46298E+04      13   0.73056E-02   0.27370E-04 
c  VelocityZ    0.46298E+04      13   0.73056E-02   0.53836E-04 
c  TurbEner     0.59778E+01      13   0.10653E-03   0.13817E-08 
c  Dissip       0.15469E+01      15   0.13308E-02   0.22139E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.42           54516           26776           27270
v  Velocity[x]            0.29265          2.0042         0.90808         0.90984
v  Velocity[y]           -0.36702         0.70199      0.00055163      0.00033136
v  Velocity[z]           -0.42087         0.50471      -0.0012521      -0.0013697
v  TurbEner             0.0010109        0.015283       0.0032861       0.0033456
v  Dissip              9.2088e-05        0.033285      0.00045311      0.00039153
v  TurbVisc               0.16538          11.319          4.7121          5.2733
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              261:        0.96366E-01

===============================================================


 INSTANT    0.262000000E+03   TIME STEP NUMBER             262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001046E+04
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 :  0.23788E+00 0.13243E+01
   Friction velocity        uet   :  0.14231E-01 0.78944E-01
   Friction velocity        uk    :  0.17415E-01 0.38772E-01
   Dimensionless distance   yplus :  0.42847E+03 0.95333E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63121E+01      54   0.13519E-02   0.20701E-01 
c  VelocityX    0.46298E+04      12   0.65462E-02   0.39181E-03 
c  VelocityY    0.46298E+04      12   0.65462E-02   0.42140E-04 
c  VelocityZ    0.46298E+04      12   0.65462E-02   0.14281E-03 
c  TurbEner     0.59757E+01      14   0.14406E-03   0.22973E-08 
c  Dissip       0.14988E+01      17   0.27234E-02   0.99923E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.46           54522           26776           27270
v  Velocity[x]             0.2927          2.0848         0.90806         0.90982
v  Velocity[y]           -0.38244         0.69458      0.00055404      0.00033405
v  Velocity[z]           -0.42161         0.51175       -0.001242      -0.0013642
v  TurbEner             0.0010108        0.014672       0.0032858       0.0033454
v  Dissip              9.2035e-05        0.031518      0.00045266      0.00039121
v  TurbVisc               0.16489          11.348           4.712          5.2732
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              262:        0.95865E-01

===============================================================


 INSTANT    0.263000000E+03   TIME STEP NUMBER             263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000078E+04
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 :  0.23798E+00 0.12168E+01
   Friction velocity        uet   :  0.14236E-01 0.72532E-01
   Friction velocity        uk    :  0.17414E-01 0.38780E-01
   Dimensionless distance   yplus :  0.42753E+03 0.95298E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57861E+01      55   0.12870E-02   0.18958E-01 
c  VelocityX    0.46297E+04      12   0.61371E-02   0.34743E-03 
c  VelocityY    0.46297E+04      12   0.61371E-02   0.26312E-04 
c  VelocityZ    0.46297E+04      12   0.61371E-02   0.42166E-04 
c  TurbEner     0.59755E+01      13   0.65908E-04   0.87135E-09 
c  Dissip       0.14967E+01      14   0.68876E-03   0.66043E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.41           54531           26775           27269
v  Velocity[x]            0.29286          2.1398         0.90805         0.90982
v  Velocity[y]            -0.3669         0.70069      0.00055642      0.00033324
v  Velocity[z]           -0.42265         0.50565      -0.0012488      -0.0013671
v  TurbEner             0.0010116        0.014586       0.0032854        0.003345
v  Dissip              9.2017e-05        0.031096      0.00045244      0.00039104
v  TurbVisc               0.16454          11.392          4.7118          5.2731
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              263:        0.95884E-01

===============================================================


 INSTANT    0.264000000E+03   TIME STEP NUMBER             264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001047E+04
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 :  0.23753E+00 0.13259E+01
   Friction velocity        uet   :  0.14209E-01 0.79031E-01
   Friction velocity        uk    :  0.17421E-01 0.38821E-01
   Dimensionless distance   yplus :  0.42814E+03 0.95278E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54974E+01      55   0.11927E-02   0.18030E-01 
c  VelocityX    0.46298E+04      13   0.65866E-02   0.26288E-03 
c  VelocityY    0.46298E+04      13   0.65866E-02   0.20110E-04 
c  VelocityZ    0.46298E+04      13   0.65866E-02   0.29075E-04 
c  TurbEner     0.59761E+01      12   0.78656E-04   0.85248E-09 
c  Dissip       0.15133E+01      15   0.68163E-03   0.10892E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.91           54540           26775           27269
v  Velocity[x]            0.29271          2.1795         0.90805         0.90983
v  Velocity[y]           -0.38285         0.69394      0.00055073      0.00033072
v  Velocity[z]           -0.42123         0.51048      -0.0012484      -0.0013689
v  TurbEner             0.0010073        0.014684       0.0032853       0.0033449
v  Dissip              9.1981e-05        0.031269      0.00045246      0.00039105
v  TurbVisc               0.16488          11.374          4.7117          5.2729
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              264:        0.96120E-01

===============================================================


 INSTANT    0.265000000E+03   TIME STEP NUMBER             265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001991E+04
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 :  0.23802E+00 0.12158E+01
   Friction velocity        uet   :  0.14238E-01 0.72333E-01
   Friction velocity        uk    :  0.17384E-01 0.38730E-01
   Dimensionless distance   yplus :  0.42751E+03 0.95219E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61614E+01      58   0.14111E-02   0.20197E-01 
c  VelocityX    0.46297E+04      13   0.73747E-02   0.37844E-03 
c  VelocityY    0.46297E+04      13   0.73747E-02   0.35030E-04 
c  VelocityZ    0.46297E+04      13   0.73747E-02   0.39882E-04 
c  TurbEner     0.59763E+01      13   0.11449E-03   0.12948E-08 
c  Dissip       0.15214E+01      16   0.18256E-02   0.34284E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.12           54547           26774           27269
v  Velocity[x]            0.29284          2.0106         0.90807         0.90984
v  Velocity[y]           -0.36742         0.70249      0.00055201      0.00033113
v  Velocity[z]           -0.42262         0.50433      -0.0012613      -0.0013806
v  TurbEner             0.0010095        0.015224       0.0032853       0.0033449
v  Dissip              9.2013e-05        0.032682      0.00045255      0.00039112
v  TurbVisc               0.16435          11.377          4.7116          5.2728
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              265:        0.96640E-01

===============================================================


 INSTANT    0.266000000E+03   TIME STEP NUMBER             266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002058E+04
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 :  0.23765E+00 0.13251E+01
   Friction velocity        uet   :  0.14216E-01 0.78987E-01
   Friction velocity        uk    :  0.17403E-01 0.38746E-01
   Dimensionless distance   yplus :  0.42722E+03 0.95234E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69467E+01      62   0.16244E-02   0.22762E-01 
c  VelocityX    0.46298E+04      12   0.72107E-02   0.43194E-03 
c  VelocityY    0.46298E+04      12   0.72107E-02   0.46159E-04 
c  VelocityZ    0.46298E+04      12   0.72107E-02   0.11140E-03 
c  TurbEner     0.59753E+01      13   0.13579E-03   0.19152E-08 
c  Dissip       0.14903E+01      16   0.22863E-02   0.73885E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -172.3           54538           26774           27268
v  Velocity[x]            0.29268          2.0942         0.90806         0.90984
v  Velocity[y]            -0.3823         0.69341      0.00056243      0.00034243
v  Velocity[z]           -0.42009         0.51183       -0.001229      -0.0013514
v  TurbEner             0.0010097        0.014663       0.0032851       0.0033447
v  Dissip              9.1991e-05        0.031231      0.00045224      0.00039092
v  TurbVisc               0.16426          11.348          4.7115          5.2727
v  total_pressure           83075      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              266:        0.96452E-01

===============================================================


 INSTANT    0.267000000E+03   TIME STEP NUMBER             267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001412E+04
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 :  0.23750E+00 0.12158E+01
   Friction velocity        uet   :  0.14207E-01 0.72474E-01
   Friction velocity        uk    :  0.17405E-01 0.38779E-01
   Dimensionless distance   yplus :  0.42770E+03 0.95249E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64094E+01      67   0.15466E-02   0.21009E-01 
c  VelocityX    0.46297E+04      12   0.68287E-02   0.42181E-03 
c  VelocityY    0.46297E+04      12   0.68287E-02   0.34567E-04 
c  VelocityZ    0.46297E+04      12   0.68287E-02   0.56017E-04 
c  TurbEner     0.59754E+01      13   0.76294E-04   0.10703E-08 
c  Dissip       0.14846E+01      14   0.70651E-03   0.63969E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.19           54511           26774           27268
v  Velocity[x]             0.2925          2.1439         0.90808         0.90985
v  Velocity[y]           -0.36602          0.6995      0.00056168      0.00034248
v  Velocity[z]            -0.4207         0.50656      -0.0012428      -0.0013611
v  TurbEner             0.0010064         0.01454       0.0032849       0.0033446
v  Dissip              9.2021e-05        0.030771      0.00045209      0.00039081
v  TurbVisc               0.16446          11.348          4.7114          5.2726
v  total_pressure           83080      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              267:        0.97836E-01

===============================================================


 INSTANT    0.268000000E+03   TIME STEP NUMBER             268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000640E+04
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 :  0.23778E+00 0.13243E+01
   Friction velocity        uet   :  0.14223E-01 0.78942E-01
   Friction velocity        uk    :  0.17376E-01 0.38804E-01
   Dimensionless distance   yplus :  0.42740E+03 0.95233E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60513E+01      55   0.12118E-02   0.19837E-01 
c  VelocityX    0.46298E+04      12   0.76203E-02   0.37950E-03 
c  VelocityY    0.46298E+04      12   0.76203E-02   0.25216E-04 
c  VelocityZ    0.46298E+04      12   0.76203E-02   0.33451E-04 
c  TurbEner     0.59754E+01      13   0.72107E-04   0.11276E-08 
c  Dissip       0.14992E+01      14   0.57324E-03   0.80065E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.43           54518           26774           27268
v  Velocity[x]            0.29282          2.1832         0.90805         0.90982
v  Velocity[y]           -0.38226         0.69308      0.00055505      0.00033627
v  Velocity[z]           -0.42312         0.51105      -0.0012388      -0.0013589
v  TurbEner             0.0010069        0.014638       0.0032848       0.0033446
v  Dissip              9.2061e-05        0.030925       0.0004521      0.00039081
v  TurbVisc               0.16397          11.322          4.7113          5.2725
v  total_pressure           83074      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              268:        0.95377E-01

===============================================================


 INSTANT    0.269000000E+03   TIME STEP NUMBER             269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998984E+04
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 :  0.23779E+00 0.12137E+01
   Friction velocity        uet   :  0.14223E-01 0.72277E-01
   Friction velocity        uk    :  0.17380E-01 0.38795E-01
   Dimensionless distance   yplus :  0.42664E+03 0.95261E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66327E+01      54   0.14148E-02   0.21733E-01 
c  VelocityX    0.46297E+04      13   0.76504E-02   0.39501E-03 
c  VelocityY    0.46297E+04      13   0.76504E-02   0.43917E-04 
c  VelocityZ    0.46297E+04      13   0.76504E-02   0.43105E-04 
c  TurbEner     0.59757E+01      13   0.11976E-03   0.14063E-08 
c  Dissip       0.15084E+01      16   0.18361E-02   0.34743E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.51           54520           26774           27268
v  Velocity[x]            0.29313            2.01         0.90807         0.90984
v  Velocity[y]           -0.36772         0.70189      0.00055626      0.00033345
v  Velocity[z]           -0.41973         0.50412      -0.0012482      -0.0013651
v  TurbEner              0.001008        0.015208       0.0032849       0.0033446
v  Dissip              9.2081e-05        0.032344      0.00045219      0.00039088
v  TurbVisc                0.1637          11.318          4.7112          5.2725
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              269:        0.95849E-01

===============================================================


 INSTANT    0.270000000E+03   TIME STEP NUMBER             270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000021E+04
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 :  0.23770E+00 0.13246E+01
   Friction velocity        uet   :  0.14217E-01 0.78966E-01
   Friction velocity        uk    :  0.17389E-01 0.38758E-01
   Dimensionless distance   yplus :  0.42741E+03 0.95270E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69908E+01      61   0.16011E-02   0.22937E-01 
c  VelocityX    0.46297E+04      12   0.70225E-02   0.39405E-03 
c  VelocityY    0.46297E+04      12   0.70225E-02   0.54839E-04 
c  VelocityZ    0.46297E+04      12   0.70225E-02   0.11916E-03 
c  TurbEner     0.59752E+01      14   0.13563E-03   0.19681E-08 
c  Dissip       0.14756E+01      17   0.22789E-02   0.73712E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.24           54513           26775           27269
v  Velocity[x]            0.29266          2.0961         0.90805         0.90982
v  Velocity[y]           -0.38247         0.69222      0.00056661      0.00034599
v  Velocity[z]           -0.42117         0.51166      -0.0012373       -0.001358
v  TurbEner             0.0010031        0.014669       0.0032848       0.0033446
v  Dissip              9.2131e-05        0.030905      0.00045194      0.00039071
v  TurbVisc               0.16409          11.334          4.7112          5.2725
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              270:        0.96813E-01

===============================================================


 INSTANT    0.271000000E+03   TIME STEP NUMBER             271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998098E+04
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 :  0.23779E+00 0.12168E+01
   Friction velocity        uet   :  0.14222E-01 0.72536E-01
   Friction velocity        uk    :  0.17348E-01 0.38651E-01
   Dimensionless distance   yplus :  0.42672E+03 0.95260E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64327E+01      57   0.13795E-02   0.21079E-01 
c  VelocityX    0.46297E+04      12   0.66805E-02   0.41325E-03 
c  VelocityY    0.46297E+04      12   0.66805E-02   0.36229E-04 
c  VelocityZ    0.46297E+04      12   0.66805E-02   0.59066E-04 
c  TurbEner     0.59745E+01      13   0.65588E-04   0.10478E-08 
c  Dissip       0.14727E+01      14   0.65453E-03   0.58403E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.16           54513           26774           27269
v  Velocity[x]            0.29274          2.1458         0.90807         0.90984
v  Velocity[y]           -0.36658         0.69947      0.00055984      0.00033729
v  Velocity[z]           -0.42261         0.50595      -0.0012531      -0.0013701
v  TurbEner             0.0010046        0.014589       0.0032846       0.0033444
v  Dissip              9.2138e-05        0.030484      0.00045181      0.00039061
v  TurbVisc               0.16348          11.381          4.7112          5.2725
v  total_pressure           83081      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              271:        0.95603E-01

===============================================================


 INSTANT    0.272000000E+03   TIME STEP NUMBER             272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000118E+04
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 :  0.23785E+00 0.13242E+01
   Friction velocity        uet   :  0.14226E-01 0.78938E-01
   Friction velocity        uk    :  0.17360E-01 0.38564E-01
   Dimensionless distance   yplus :  0.42626E+03 0.95328E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58923E+01      59   0.12297E-02   0.19310E-01 
c  VelocityX    0.46298E+04      12   0.70019E-02   0.30334E-03 
c  VelocityY    0.46298E+04      12   0.70019E-02   0.24089E-04 
c  VelocityZ    0.46298E+04      12   0.70019E-02   0.29706E-04 
c  TurbEner     0.59757E+01      13   0.76295E-04   0.10422E-08 
c  Dissip       0.14873E+01      15   0.65798E-03   0.10365E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.71           54528           26775           27269
v  Velocity[x]            0.29271          2.1846         0.90805         0.90983
v  Velocity[y]           -0.38225         0.69242      0.00055583      0.00033194
v  Velocity[z]           -0.42099         0.51109      -0.0012419       -0.001361
v  TurbEner             0.0010044        0.014702       0.0032847       0.0033445
v  Dissip              9.2142e-05        0.030607      0.00045188      0.00039065
v  TurbVisc               0.16342          11.362          4.7111          5.2724
v  total_pressure           83075      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              272:        0.96022E-01

===============================================================


 INSTANT    0.273000000E+03   TIME STEP NUMBER             273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000689E+04
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 :  0.23791E+00 0.12164E+01
   Friction velocity        uet   :  0.14229E-01 0.72512E-01
   Friction velocity        uk    :  0.17359E-01 0.38683E-01
   Dimensionless distance   yplus :  0.42654E+03 0.95333E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63486E+01      61   0.13744E-02   0.20826E-01 
c  VelocityX    0.46297E+04      12   0.68960E-02   0.37271E-03 
c  VelocityY    0.46297E+04      12   0.68960E-02   0.43657E-04 
c  VelocityZ    0.46297E+04      12   0.68960E-02   0.39556E-04 
c  TurbEner     0.59762E+01      13   0.12303E-03   0.15835E-08 
c  Dissip       0.14969E+01      16   0.17513E-02   0.32435E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.06           54539           26775           27269
v  Velocity[x]            0.29277          2.0131         0.90807         0.90984
v  Velocity[y]           -0.36696         0.70093      0.00055579      0.00033256
v  Velocity[z]           -0.42235         0.50469      -0.0012529      -0.0013705
v  TurbEner             0.0010017        0.015293       0.0032847       0.0033445
v  Dissip              9.2144e-05        0.031965        0.000452      0.00039073
v  TurbVisc               0.16363          11.364          4.7113          5.2725
v  total_pressure           83082      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              273:        0.96302E-01

===============================================================


 INSTANT    0.274000000E+03   TIME STEP NUMBER             274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999301E+04
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 :  0.23771E+00 0.13234E+01
   Friction velocity        uet   :  0.14217E-01 0.78884E-01
   Friction velocity        uk    :  0.17336E-01 0.38767E-01
   Dimensionless distance   yplus :  0.42634E+03 0.95326E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58175E+01      56   0.12092E-02   0.19070E-01 
c  VelocityX    0.46297E+04      12   0.68510E-02   0.32654E-03 
c  VelocityY    0.46297E+04      12   0.68510E-02   0.21215E-04 
c  VelocityZ    0.46297E+04      12   0.68510E-02   0.47770E-04 
c  TurbEner     0.59752E+01      13   0.12571E-03   0.18305E-08 
c  Dissip       0.14594E+01      16   0.21533E-02   0.69634E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.73           54548           26775           27270
v  Velocity[x]            0.29281          2.0925         0.90805         0.90982
v  Velocity[y]           -0.38244         0.69397      0.00054681      0.00032637
v  Velocity[z]           -0.42312          0.5117      -0.0012466      -0.0013679
v  TurbEner             0.0010031        0.014759       0.0032845       0.0033444
v  Dissip              9.2085e-05        0.030638      0.00045166       0.0003905
v  TurbVisc               0.16345          11.336          4.7112          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              274:        0.96163E-01

===============================================================


 INSTANT    0.275000000E+03   TIME STEP NUMBER             275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997413E+04
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 :  0.23774E+00 0.12164E+01
   Friction velocity        uet   :  0.14219E-01 0.72509E-01
   Friction velocity        uk    :  0.17348E-01 0.38778E-01
   Dimensionless distance   yplus :  0.42576E+03 0.95346E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61753E+01      53   0.15302E-02   0.20233E-01 
c  VelocityX    0.46297E+04      12   0.77531E-02   0.36981E-03 
c  VelocityY    0.46297E+04      12   0.77531E-02   0.29016E-04 
c  VelocityZ    0.46297E+04      12   0.77531E-02   0.49741E-04 
c  TurbEner     0.59758E+01      13   0.68395E-04   0.66930E-09 
c  Dissip       0.14670E+01      14   0.50372E-03   0.35954E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.71           54540           26775           27270
v  Velocity[x]            0.29298          2.1454         0.90806         0.90984
v  Velocity[y]           -0.36694         0.70088      0.00055845      0.00033743
v  Velocity[z]           -0.42041         0.50573      -0.0012489      -0.0013673
v  TurbEner             0.0010055        0.014675       0.0032845       0.0033444
v  Dissip              9.2051e-05        0.030336      0.00045153       0.0003904
v  TurbVisc               0.16329          11.332          4.7112          5.2725
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              275:        0.95082E-01

===============================================================


 INSTANT    0.276000000E+03   TIME STEP NUMBER             276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998460E+04
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 :  0.23734E+00 0.13253E+01
   Friction velocity        uet   :  0.14195E-01 0.78995E-01
   Friction velocity        uk    :  0.17368E-01 0.38734E-01
   Dimensionless distance   yplus :  0.42678E+03 0.95332E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69963E+01      55   0.16402E-02   0.22937E-01 
c  VelocityX    0.46298E+04      12   0.70721E-02   0.42131E-03 
c  VelocityY    0.46298E+04      12   0.70721E-02   0.31479E-04 
c  VelocityZ    0.46298E+04      12   0.70721E-02   0.97764E-04 
c  TurbEner     0.59770E+01      13   0.82563E-04   0.12803E-08 
c  Dissip       0.14877E+01      15   0.79410E-03   0.15485E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.46           54525           26776           27270
v  Velocity[x]            0.29217          2.1895         0.90807         0.90984
v  Velocity[y]           -0.38281         0.69431      0.00056194      0.00034324
v  Velocity[z]           -0.42049         0.51053      -0.0012315       -0.001352
v  TurbEner             0.0010018        0.014783       0.0032847       0.0033445
v  Dissip              9.2024e-05        0.030552      0.00045169      0.00039052
v  TurbVisc               0.16388          11.358          4.7112          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              276:        0.95633E-01

===============================================================


 INSTANT    0.277000000E+03   TIME STEP NUMBER             277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998992E+04
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 :  0.23784E+00 0.12134E+01
   Friction velocity        uet   :  0.14225E-01 0.72332E-01
   Friction velocity        uk    :  0.17336E-01 0.38661E-01
   Dimensionless distance   yplus :  0.42632E+03 0.95392E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64788E+01      57   0.14707E-02   0.21239E-01 
c  VelocityX    0.46298E+04      13   0.70204E-02   0.39118E-03 
c  VelocityY    0.46298E+04      13   0.70204E-02   0.30321E-04 
c  VelocityZ    0.46298E+04      13   0.70204E-02   0.48005E-04 
c  TurbEner     0.59770E+01      13   0.12803E-03   0.16630E-08 
c  Dissip       0.15030E+01      16   0.21711E-02   0.52727E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.87           54525           26776           27270
v  Velocity[x]            0.29279           2.022         0.90807         0.90983
v  Velocity[y]           -0.36738         0.70287       0.0005595        0.000336
v  Velocity[z]            -0.4211         0.50432      -0.0012538      -0.0013704
v  TurbEner             0.0010045        0.015415       0.0032849       0.0033447
v  Dissip              9.2046e-05        0.032236      0.00045189      0.00039068
v  TurbVisc               0.16351          11.341          4.7113          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              277:        0.97361E-01

===============================================================


 INSTANT    0.278000000E+03   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001109E+04
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 :  0.23809E+00 0.13254E+01
   Friction velocity        uet   :  0.14241E-01 0.79004E-01
   Friction velocity        uk    :  0.17359E-01 0.38730E-01
   Dimensionless distance   yplus :  0.42609E+03 0.95417E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64775E+01      57   0.13563E-02   0.21233E-01 
c  VelocityX    0.46298E+04      12   0.72446E-02   0.34862E-03 
c  VelocityY    0.46298E+04      12   0.72446E-02   0.23658E-04 
c  VelocityZ    0.46298E+04      12   0.72446E-02   0.49093E-04 
c  TurbEner     0.59761E+01      14   0.12629E-03   0.20069E-08 
c  Dissip       0.14740E+01      16   0.19358E-02   0.58081E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -167.5           54533           26776           27270
v  Velocity[x]            0.29331          2.0946         0.90806         0.90984
v  Velocity[y]           -0.38228         0.69321      0.00055627      0.00033263
v  Velocity[z]           -0.42139          0.5119      -0.0012504      -0.0013696
v  TurbEner             0.0010047        0.014873       0.0032848       0.0033446
v  Dissip               9.212e-05        0.031045      0.00045166      0.00039051
v  TurbVisc               0.16349          11.348          4.7114          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              278:        0.95884E-01

===============================================================


 INSTANT    0.279000000E+03   TIME STEP NUMBER             279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998862E+04
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 :  0.23766E+00 0.12172E+01
   Friction velocity        uet   :  0.14216E-01 0.72555E-01
   Friction velocity        uk    :  0.17361E-01 0.38806E-01
   Dimensionless distance   yplus :  0.42660E+03 0.95336E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61057E+01      56   0.11306E-02   0.20007E-01 
c  VelocityX    0.46299E+04      12   0.63504E-02   0.37508E-03 
c  VelocityY    0.46299E+04      12   0.63504E-02   0.27676E-04 
c  VelocityZ    0.46299E+04      12   0.63504E-02   0.49414E-04 
c  TurbEner     0.59765E+01      12   0.70961E-04   0.77001E-09 
c  Dissip       0.14809E+01      13   0.52262E-03   0.40453E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.14           54541           26775           27269
v  Velocity[x]            0.29271          2.1445         0.90807         0.90984
v  Velocity[y]           -0.36607         0.70122      0.00055239      0.00032874
v  Velocity[z]            -0.4222         0.50651      -0.0012559      -0.0013718
v  TurbEner             0.0010017        0.014752       0.0032848       0.0033447
v  Dissip              9.2122e-05        0.030752      0.00045167      0.00039051
v  TurbVisc               0.16379          11.384          4.7114          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              279:        0.95692E-01

===============================================================


 INSTANT    0.280000000E+03   TIME STEP NUMBER             280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001373E+04
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 :  0.23776E+00 0.13244E+01
   Friction velocity        uet   :  0.14222E-01 0.78947E-01
   Friction velocity        uk    :  0.17335E-01 0.38817E-01
   Dimensionless distance   yplus :  0.42637E+03 0.95336E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59090E+01      52   0.12056E-02   0.19370E-01 
c  VelocityX    0.46298E+04      12   0.69949E-02   0.30130E-03 
c  VelocityY    0.46298E+04      12   0.69949E-02   0.37217E-04 
c  VelocityZ    0.46298E+04      12   0.69949E-02   0.80145E-04 
c  TurbEner     0.59779E+01      13   0.75956E-04   0.10276E-08 
c  Dissip       0.15019E+01      15   0.77298E-03   0.14329E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.67           54548           26775           27270
v  Velocity[x]             0.2926          2.1857         0.90807         0.90985
v  Velocity[y]            -0.3823         0.69591      0.00055614      0.00033536
v  Velocity[z]            -0.4221         0.51112      -0.0012446      -0.0013668
v  TurbEner             0.0010024        0.014846       0.0032852        0.003345
v  Dissip              9.2124e-05        0.030976       0.0004519      0.00039068
v  TurbVisc               0.16351          11.363          4.7114          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              280:        0.95320E-01

===============================================================


 INSTANT    0.281000000E+03   TIME STEP NUMBER             281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999062E+04
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 :  0.23787E+00 0.12137E+01
   Friction velocity        uet   :  0.14229E-01 0.72351E-01
   Friction velocity        uk    :  0.17341E-01 0.38810E-01
   Dimensionless distance   yplus :  0.42570E+03 0.95334E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60014E+01      64   0.16399E-02   0.19682E-01 
c  VelocityX    0.46299E+04      13   0.74250E-02   0.37064E-03 
c  VelocityY    0.46299E+04      13   0.74250E-02   0.25535E-04 
c  VelocityZ    0.46299E+04      13   0.74250E-02   0.41065E-04 
c  TurbEner     0.59787E+01      13   0.12243E-03   0.13939E-08 
c  Dissip       0.15167E+01      16   0.20438E-02   0.46399E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.31           54540           26775           27270
v  Velocity[x]            0.29292          2.0183         0.90807         0.90985
v  Velocity[y]           -0.36776         0.70491      0.00055956      0.00033665
v  Velocity[z]           -0.42077         0.50419      -0.0012449      -0.0013623
v  TurbEner             0.0010042         0.01543       0.0032855       0.0033452
v  Dissip              9.2096e-05        0.032561      0.00045218      0.00039089
v  TurbVisc               0.16334          11.363          4.7116          5.2729
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              281:        0.98437E-01

===============================================================


 INSTANT    0.282000000E+03   TIME STEP NUMBER             282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999659E+04
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 :  0.23732E+00 0.13249E+01
   Friction velocity        uet   :  0.14197E-01 0.78979E-01
   Friction velocity        uk    :  0.17357E-01 0.38750E-01
   Dimensionless distance   yplus :  0.42664E+03 0.95304E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58487E+01      57   0.16046E-02   0.19187E-01 
c  VelocityX    0.46298E+04      13   0.66122E-02   0.33700E-03 
c  VelocityY    0.46298E+04      13   0.66122E-02   0.22651E-04 
c  VelocityZ    0.46298E+04      13   0.66122E-02   0.54366E-04 
c  TurbEner     0.59776E+01      14   0.14013E-03   0.23645E-08 
c  Dissip       0.14817E+01      16   0.21933E-02   0.73111E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.38           54516           26776           27271
v  Velocity[x]            0.29274          2.0918         0.90806         0.90983
v  Velocity[y]           -0.38254         0.69223       0.0005618      0.00034197
v  Velocity[z]           -0.42027         0.51166      -0.0012335      -0.0013531
v  TurbEner             0.0010001        0.014844       0.0032856       0.0033453
v  Dissip              9.2087e-05        0.031196      0.00045203       0.0003908
v  TurbVisc               0.16393          11.335          4.7116          5.2729
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              282:        0.97058E-01

===============================================================


 INSTANT    0.283000000E+03   TIME STEP NUMBER             283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998904E+04
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 :  0.23793E+00 0.12180E+01
   Friction velocity        uet   :  0.14234E-01 0.72598E-01
   Friction velocity        uk    :  0.17321E-01 0.38703E-01
   Dimensionless distance   yplus :  0.42611E+03 0.95370E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57232E+01      52   0.11626E-02   0.18760E-01 
c  VelocityX    0.46299E+04      12   0.69195E-02   0.36516E-03 
c  VelocityY    0.46299E+04      12   0.69195E-02   0.29298E-04 
c  VelocityZ    0.46299E+04      12   0.69195E-02   0.46693E-04 
c  TurbEner     0.59770E+01      13   0.68400E-04   0.95137E-09 
c  Dissip       0.14830E+01      14   0.59799E-03   0.45703E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.76           54523           26776           27270
v  Velocity[x]             0.2927          2.1432         0.90806         0.90983
v  Velocity[y]           -0.36656         0.70098      0.00056221      0.00033991
v  Velocity[z]           -0.42189         0.50603      -0.0012497      -0.0013698
v  TurbEner              0.001003        0.014712       0.0032856       0.0033453
v  Dissip              9.2149e-05        0.030801      0.00045201      0.00039078
v  TurbVisc               0.16359           11.33          4.7116          5.2729
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              283:        0.95420E-01

===============================================================


 INSTANT    0.284000000E+03   TIME STEP NUMBER             284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001289E+04
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 :  0.23782E+00 0.13235E+01
   Friction velocity        uet   :  0.14227E-01 0.78885E-01
   Friction velocity        uk    :  0.17346E-01 0.38777E-01
   Dimensionless distance   yplus :  0.42586E+03 0.95399E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60528E+01      58   0.11836E-02   0.19840E-01 
c  VelocityX    0.46299E+04      12   0.66609E-02   0.32870E-03 
c  VelocityY    0.46299E+04      12   0.66609E-02   0.42661E-04 
c  VelocityZ    0.46299E+04      12   0.66609E-02   0.76051E-04 
c  TurbEner     0.59778E+01      13   0.74305E-04   0.10472E-08 
c  Dissip       0.15024E+01      15   0.73426E-03   0.12721E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.26           54533           26776           27270
v  Velocity[x]            0.29293          2.1825         0.90805         0.90982
v  Velocity[y]           -0.38228         0.69534      0.00055714      0.00033598
v  Velocity[z]           -0.42146         0.51102      -0.0012362      -0.0013567
v  TurbEner              0.001004        0.014842       0.0032856       0.0033454
v  Dissip              9.2179e-05        0.031038      0.00045216      0.00039088
v  TurbVisc               0.16367          11.355          4.7116          5.2729
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              284:        0.95991E-01

===============================================================


 INSTANT    0.285000000E+03   TIME STEP NUMBER             285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999664E+04
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 :  0.23770E+00 0.12479E+01
   Friction velocity        uet   :  0.14219E-01 0.72780E-01
   Friction velocity        uk    :  0.17355E-01 0.38807E-01
   Dimensionless distance   yplus :  0.42645E+03 0.95350E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58118E+01      54   0.14076E-02   0.19047E-01 
c  VelocityX    0.46298E+04      12   0.69552E-02   0.39109E-03 
c  VelocityY    0.46298E+04      12   0.69552E-02   0.25838E-04 
c  VelocityZ    0.46298E+04      12   0.69552E-02   0.39649E-04 
c  TurbEner     0.59785E+01      13   0.12082E-03   0.12238E-08 
c  Dissip       0.15173E+01      16   0.20170E-02   0.44256E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.42           54540           26775           27270
v  Velocity[x]            0.29275          2.0163         0.90806         0.90984
v  Velocity[y]           -0.36703         0.70323      0.00055657      0.00033378
v  Velocity[z]           -0.42144         0.50466      -0.0012568      -0.0013751
v  TurbEner             0.0010028        0.015442       0.0032857       0.0033455
v  Dissip              9.2136e-05        0.032606      0.00045239      0.00039105
v  TurbVisc               0.16411          11.336          4.7116          5.2729
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              285:        0.95840E-01

===============================================================


 INSTANT    0.286000000E+03   TIME STEP NUMBER             286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001073E+04
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 :  0.23780E+00 0.13244E+01
   Friction velocity        uet   :  0.14225E-01 0.78937E-01
   Friction velocity        uk    :  0.17345E-01 0.38804E-01
   Dimensionless distance   yplus :  0.42653E+03 0.95372E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55856E+01      55   0.13173E-02   0.18314E-01 
c  VelocityX    0.46299E+04      12   0.65464E-02   0.35463E-03 
c  VelocityY    0.46299E+04      12   0.65464E-02   0.23501E-04 
c  VelocityZ    0.46299E+04      12   0.65464E-02   0.48882E-04 
c  TurbEner     0.59773E+01      13   0.13777E-03   0.17918E-08 
c  Dissip       0.14805E+01      16   0.22292E-02   0.72252E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.8           54548           26775           27270
v  Velocity[x]            0.29254          2.0898         0.90805         0.90983
v  Velocity[y]           -0.38244         0.69536      0.00055201      0.00033028
v  Velocity[z]           -0.42247         0.51167      -0.0012481       -0.001369
v  TurbEner             0.0010056        0.014861       0.0032857       0.0033455
v  Dissip              9.2101e-05        0.031183      0.00045218      0.00039092
v  TurbVisc               0.16416          11.349          4.7115          5.2729
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              286:        0.95809E-01

===============================================================


 INSTANT    0.287000000E+03   TIME STEP NUMBER             287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000108E+04
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 :  0.23779E+00 0.12161E+01
   Friction velocity        uet   :  0.14224E-01 0.72485E-01
   Friction velocity        uk    :  0.17369E-01 0.38772E-01
   Dimensionless distance   yplus :  0.42623E+03 0.95346E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60484E+01      56   0.15067E-02   0.19820E-01 
c  VelocityX    0.46299E+04      12   0.69610E-02   0.31370E-03 
c  VelocityY    0.46299E+04      12   0.69610E-02   0.25238E-04 
c  VelocityZ    0.46299E+04      12   0.69610E-02   0.52567E-04 
c  TurbEner     0.59774E+01      13   0.65841E-04   0.70339E-09 
c  Dissip       0.14803E+01      14   0.62070E-03   0.44961E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.38           54540           26776           27270
v  Velocity[x]            0.29308          2.1396         0.90807         0.90985
v  Velocity[y]           -0.36691         0.70148       0.0005561      0.00033159
v  Velocity[z]           -0.41909         0.50558      -0.0012484       -0.001368
v  TurbEner             0.0010097        0.014737       0.0032857       0.0033454
v  Dissip              9.2049e-05        0.030766      0.00045209      0.00039085
v  TurbVisc                0.1641           11.33          4.7116          5.2729
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              287:        0.95649E-01

===============================================================


 INSTANT    0.288000000E+03   TIME STEP NUMBER             288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998349E+04
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 :  0.23747E+00 0.13251E+01
   Friction velocity        uet   :  0.14204E-01 0.78982E-01
   Friction velocity        uk    :  0.17404E-01 0.38794E-01
   Dimensionless distance   yplus :  0.42754E+03 0.95244E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69361E+01      62   0.15643E-02   0.22750E-01 
c  VelocityX    0.46299E+04      12   0.71229E-02   0.37576E-03 
c  VelocityY    0.46299E+04      12   0.71229E-02   0.77855E-04 
c  VelocityZ    0.46299E+04      12   0.71229E-02   0.11041E-03 
c  TurbEner     0.59783E+01      13   0.71426E-04   0.10507E-08 
c  Dissip       0.14984E+01      15   0.63912E-03   0.10213E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.79           54522           26777           27271
v  Velocity[x]            0.29275          2.1822         0.90806         0.90983
v  Velocity[y]           -0.38288         0.69299      0.00056617      0.00034484
v  Velocity[z]           -0.42101         0.51049      -0.0012235      -0.0013464
v  TurbEner             0.0010076        0.014849       0.0032858       0.0033456
v  Dissip              9.2058e-05        0.030916      0.00045225      0.00039096
v  TurbVisc               0.16485          11.328          4.7115          5.2729
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              288:        0.96477E-01

===============================================================


 INSTANT    0.289000000E+03   TIME STEP NUMBER             289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998123E+04
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 :  0.23777E+00 0.12332E+01
   Friction velocity        uet   :  0.14223E-01 0.72454E-01
   Friction velocity        uk    :  0.17387E-01 0.38740E-01
   Dimensionless distance   yplus :  0.42738E+03 0.95223E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61062E+01      57   0.13642E-02   0.20013E-01 
c  VelocityX    0.46298E+04      12   0.65873E-02   0.44167E-03 
c  VelocityY    0.46298E+04      12   0.65873E-02   0.30131E-04 
c  VelocityZ    0.46298E+04      12   0.65873E-02   0.53430E-04 
c  TurbEner     0.59779E+01      13   0.12914E-03   0.17618E-08 
c  Dissip       0.15116E+01      16   0.20030E-02   0.45334E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.08           54525           26777           27271
v  Velocity[x]            0.29262          2.0134         0.90805         0.90982
v  Velocity[y]           -0.36735         0.70183      0.00055994      0.00033496
v  Velocity[z]           -0.42225         0.50437      -0.0012424      -0.0013627
v  TurbEner             0.0010121        0.015475       0.0032858       0.0033455
v  Dissip              9.2008e-05        0.032464      0.00045242      0.00039108
v  TurbVisc               0.16467          11.363          4.7115          5.2728
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              289:        0.96254E-01

===============================================================


 INSTANT    0.290000000E+03   TIME STEP NUMBER             290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000743E+04
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 :  0.23791E+00 0.13226E+01
   Friction velocity        uet   :  0.14230E-01 0.78834E-01
   Friction velocity        uk    :  0.17425E-01 0.38741E-01
   Dimensionless distance   yplus :  0.42745E+03 0.95213E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61914E+01      68   0.13201E-02   0.20288E-01 
c  VelocityX    0.46298E+04      12   0.61905E-02   0.35192E-03 
c  VelocityY    0.46298E+04      12   0.61905E-02   0.26347E-04 
c  VelocityZ    0.46298E+04      12   0.61905E-02   0.51006E-04 
c  TurbEner     0.59766E+01      14   0.13090E-03   0.18973E-08 
c  Dissip       0.14748E+01      16   0.22424E-02   0.73787E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.51           54532           26776           27270
v  Velocity[x]            0.29285          2.0909         0.90804         0.90982
v  Velocity[y]           -0.38225         0.69372      0.00055505      0.00033315
v  Velocity[z]           -0.42097         0.51188      -0.0012403      -0.0013628
v  TurbEner             0.0010142          0.0149       0.0032857       0.0033454
v  Dissip              9.2013e-05        0.031033       0.0004522      0.00039093
v  TurbVisc               0.16472           11.33          4.7114          5.2727
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              290:        0.99084E-01

===============================================================


 INSTANT    0.291000000E+03   TIME STEP NUMBER             291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000655E+04
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 :  0.23778E+00 0.12159E+01
   Friction velocity        uet   :  0.14222E-01 0.72490E-01
   Friction velocity        uk    :  0.17443E-01 0.38749E-01
   Dimensionless distance   yplus :  0.42828E+03 0.95178E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57500E+01      59   0.12671E-02   0.18857E-01 
c  VelocityX    0.46299E+04      12   0.61633E-02   0.30718E-03 
c  VelocityY    0.46299E+04      12   0.61633E-02   0.23300E-04 
c  VelocityZ    0.46299E+04      12   0.61633E-02   0.37241E-04 
c  TurbEner     0.59768E+01      12   0.68994E-04   0.63579E-09 
c  Dissip       0.14769E+01      13   0.54320E-03   0.38779E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.3           54540           26776           27270
v  Velocity[x]            0.29293          2.1409         0.90806         0.90984
v  Velocity[y]           -0.36603         0.70032      0.00054884      0.00032469
v  Velocity[z]           -0.42133         0.50661      -0.0012469      -0.0013677
v  TurbEner             0.0010131        0.014795       0.0032857       0.0033454
v  Dissip              9.2005e-05        0.030702      0.00045221      0.00039094
v  TurbVisc               0.16513           11.32          4.7114          5.2727
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              291:        0.95915E-01

===============================================================


 INSTANT    0.292000000E+03   TIME STEP NUMBER             292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002376E+04
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 :  0.23787E+00 0.13243E+01
   Friction velocity        uet   :  0.14227E-01 0.78945E-01
   Friction velocity        uk    :  0.17433E-01 0.38769E-01
   Dimensionless distance   yplus :  0.42840E+03 0.95243E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62152E+01      54   0.12727E-02   0.20378E-01 
c  VelocityX    0.46299E+04      12   0.68734E-02   0.30805E-03 
c  VelocityY    0.46299E+04      12   0.68734E-02   0.52169E-04 
c  VelocityZ    0.46299E+04      12   0.68734E-02   0.37905E-04 
c  TurbEner     0.59775E+01      12   0.67025E-04   0.71521E-09 
c  Dissip       0.14967E+01      15   0.71438E-03   0.11718E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.17           54550           26776           27270
v  Velocity[x]            0.29273          2.1795         0.90806         0.90983
v  Velocity[y]           -0.38229         0.69388      0.00055283      0.00033151
v  Velocity[z]           -0.42283         0.51107      -0.0012343      -0.0013579
v  TurbEner             0.0010151        0.014907       0.0032857       0.0033454
v  Dissip              9.2029e-05        0.030958      0.00045233      0.00039101
v  TurbVisc               0.16505          11.345          4.7114          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              292:        0.95665E-01

===============================================================


 INSTANT    0.293000000E+03   TIME STEP NUMBER             293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998255E+04
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 :  0.23756E+00 0.12309E+01
   Friction velocity        uet   :  0.14208E-01 0.72263E-01
   Friction velocity        uk    :  0.17451E-01 0.38776E-01
   Dimensionless distance   yplus :  0.42799E+03 0.95297E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60696E+01      58   0.16982E-02   0.19890E-01 
c  VelocityX    0.46298E+04      13   0.75290E-02   0.40226E-03 
c  VelocityY    0.46298E+04      13   0.75290E-02   0.28441E-04 
c  VelocityZ    0.46298E+04      13   0.75290E-02   0.49811E-04 
c  TurbEner     0.59782E+01      13   0.12065E-03   0.12311E-08 
c  Dissip       0.15124E+01      16   0.20174E-02   0.45208E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.2           54540           26776           27270
v  Velocity[x]            0.29299          2.0161         0.90807         0.90985
v  Velocity[y]           -0.36776          0.7026      0.00055507      0.00032946
v  Velocity[z]           -0.42039         0.50409      -0.0012457      -0.0013662
v  TurbEner             0.0010172         0.01551       0.0032859       0.0033455
v  Dissip              9.2047e-05        0.032529      0.00045256      0.00039117
v  TurbVisc                0.1648           11.39          4.7114          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              293:        0.96466E-01

===============================================================


 INSTANT    0.294000000E+03   TIME STEP NUMBER             294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001094E+04
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 :  0.23736E+00 0.13246E+01
   Friction velocity        uet   :  0.14196E-01 0.78960E-01
   Friction velocity        uk    :  0.17469E-01 0.38796E-01
   Dimensionless distance   yplus :  0.42896E+03 0.95281E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70442E+01      56   0.15879E-02   0.23095E-01 
c  VelocityX    0.46299E+04      12   0.68160E-02   0.45766E-03 
c  VelocityY    0.46299E+04      12   0.68160E-02   0.33550E-04 
c  VelocityZ    0.46299E+04      12   0.68160E-02   0.11383E-03 
c  TurbEner     0.59772E+01      14   0.13319E-03   0.21128E-08 
c  Dissip       0.14798E+01      16   0.22385E-02   0.72259E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.34           54516           26776           27270
v  Velocity[x]            0.29267           2.096         0.90806         0.90983
v  Velocity[y]           -0.38252         0.69228      0.00056082      0.00034128
v  Velocity[z]           -0.42043         0.51162      -0.0012264      -0.0013481
v  TurbEner             0.0010138        0.014928       0.0032858       0.0033455
v  Dissip              9.2052e-05        0.031074      0.00045237      0.00039105
v  TurbVisc               0.16528          11.374          4.7114          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              294:        0.95903E-01

===============================================================


 INSTANT    0.295000000E+03   TIME STEP NUMBER             295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999579E+04
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 :  0.23791E+00 0.12167E+01
   Friction velocity        uet   :  0.14229E-01 0.72526E-01
   Friction velocity        uk    :  0.17439E-01 0.38715E-01
   Dimensionless distance   yplus :  0.42858E+03 0.95342E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61219E+01      55   0.13333E-02   0.20074E-01 
c  VelocityX    0.46298E+04      12   0.70350E-02   0.36984E-03 
c  VelocityY    0.46298E+04      12   0.70350E-02   0.32833E-04 
c  VelocityZ    0.46298E+04      12   0.70350E-02   0.49815E-04 
c  TurbEner     0.59769E+01      13   0.65802E-04   0.10490E-08 
c  Dissip       0.14776E+01      14   0.62797E-03   0.52930E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.83           54522           26776           27270
v  Velocity[x]            0.29273          2.1466         0.90807         0.90984
v  Velocity[y]           -0.36659         0.69922      0.00055908      0.00033357
v  Velocity[z]           -0.42116         0.50595      -0.0012457      -0.0013653
v  TurbEner             0.0010168        0.014805       0.0032859       0.0033456
v  Dissip              9.2052e-05        0.030666      0.00045234      0.00039103
v  TurbVisc               0.16495          11.324          4.7114          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              295:        0.95623E-01

===============================================================


 INSTANT    0.296000000E+03   TIME STEP NUMBER             296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999160E+04
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 :  0.23798E+00 0.13232E+01
   Friction velocity        uet   :  0.14233E-01 0.78874E-01
   Friction velocity        uk    :  0.17466E-01 0.38740E-01
   Dimensionless distance   yplus :  0.42849E+03 0.95399E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63891E+01      58   0.11964E-02   0.20939E-01 
c  VelocityX    0.46298E+04      12   0.71360E-02   0.35835E-03 
c  VelocityY    0.46298E+04      12   0.71360E-02   0.22915E-04 
c  VelocityZ    0.46298E+04      12   0.71360E-02   0.35787E-04 
c  TurbEner     0.59777E+01      13   0.67717E-04   0.83440E-09 
c  Dissip       0.14953E+01      15   0.65732E-03   0.10201E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.64           54532           26776           27270
v  Velocity[x]             0.2929          2.1849         0.90806         0.90983
v  Velocity[y]           -0.38228         0.69229      0.00055635      0.00033472
v  Velocity[z]           -0.42064         0.51103      -0.0012457      -0.0013668
v  TurbEner             0.0010176        0.014907       0.0032861       0.0033456
v  Dissip              9.2011e-05        0.030874      0.00045246       0.0003911
v  TurbVisc               0.16492          11.313          4.7115          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              296:        0.95796E-01

===============================================================


 INSTANT    0.297000000E+03   TIME STEP NUMBER             297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000579E+04
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 :  0.23784E+00 0.12156E+01
   Friction velocity        uet   :  0.14225E-01 0.72468E-01
   Friction velocity        uk    :  0.17472E-01 0.38793E-01
   Dimensionless distance   yplus :  0.42916E+03 0.95387E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64699E+01      60   0.15128E-02   0.21216E-01 
c  VelocityX    0.46298E+04      13   0.68700E-02   0.39124E-03 
c  VelocityY    0.46298E+04      13   0.68700E-02   0.49740E-04 
c  VelocityZ    0.46298E+04      13   0.68700E-02   0.33883E-04 
c  TurbEner     0.59783E+01      13   0.12016E-03   0.13956E-08 
c  Dissip       0.15071E+01      16   0.18171E-02   0.35607E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.09           54540           26776           27270
v  Velocity[x]            0.29276          2.0137         0.90809         0.90986
v  Velocity[y]           -0.36695         0.70077      0.00055526      0.00033033
v  Velocity[z]           -0.42256          0.5047      -0.0012521      -0.0013695
v  TurbEner             0.0010149        0.015484       0.0032862       0.0033458
v  Dissip              9.2028e-05        0.032299      0.00045265      0.00039124
v  TurbVisc               0.16527          11.345          4.7116          5.2729
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              297:        0.97454E-01

===============================================================


 INSTANT    0.298000000E+03   TIME STEP NUMBER             298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000270E+04
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 :  0.23758E+00 0.13230E+01
   Friction velocity        uet   :  0.14209E-01 0.78857E-01
   Friction velocity        uk    :  0.17449E-01 0.38842E-01
   Dimensionless distance   yplus :  0.42901E+03 0.95425E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61274E+01      57   0.13103E-02   0.20086E-01 
c  VelocityX    0.46298E+04      12   0.70491E-02   0.34925E-03 
c  VelocityY    0.46298E+04      12   0.70491E-02   0.23444E-04 
c  VelocityZ    0.46298E+04      12   0.70491E-02   0.53508E-04 
c  TurbEner     0.59772E+01      14   0.13239E-03   0.20442E-08 
c  Dissip       0.14702E+01      16   0.21359E-02   0.68712E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.76           54549           26777           27271
v  Velocity[x]            0.29251          2.0906         0.90805         0.90983
v  Velocity[y]           -0.38234          0.6935      0.00055422      0.00033383
v  Velocity[z]           -0.42015         0.51173      -0.0012562      -0.0013785
v  TurbEner             0.0010164        0.014934       0.0032862       0.0033457
v  Dissip              9.2022e-05         0.03095      0.00045239      0.00039105
v  TurbVisc               0.16507           11.33          4.7116          5.2729
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              298:        0.96078E-01

===============================================================


 INSTANT    0.299000000E+03   TIME STEP NUMBER             299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399996890E+04
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 :  0.23771E+00 0.12335E+01
   Friction velocity        uet   :  0.14217E-01 0.72466E-01
   Friction velocity        uk    :  0.17462E-01 0.38871E-01
   Dimensionless distance   yplus :  0.42843E+03 0.95438E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59852E+01      54   0.15316E-02   0.19621E-01 
c  VelocityX    0.46299E+04      12   0.64696E-02   0.36906E-03 
c  VelocityY    0.46299E+04      12   0.64696E-02   0.28113E-04 
c  VelocityZ    0.46299E+04      12   0.64696E-02   0.39701E-04 
c  TurbEner     0.59776E+01      12   0.65538E-04   0.68394E-09 
c  Dissip       0.14766E+01      14   0.50083E-03   0.33980E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.85           54541           26777           27271
v  Velocity[x]            0.29271          2.1435         0.90808         0.90985
v  Velocity[y]           -0.36684         0.70002      0.00055777      0.00033487
v  Velocity[z]           -0.41974         0.50578      -0.0012499      -0.0013664
v  TurbEner             0.0010186        0.014829       0.0032862       0.0033457
v  Dissip              9.2039e-05        0.030645      0.00045237      0.00039104
v  TurbVisc               0.16483          11.333          4.7116          5.2729
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              299:        0.95564E-01

===============================================================


 INSTANT    0.300000000E+03   TIME STEP NUMBER             300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999050E+04
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 :  0.23735E+00 0.13246E+01
   Friction velocity        uet   :  0.14195E-01 0.78958E-01
   Friction velocity        uk    :  0.17481E-01 0.38861E-01
   Dimensionless distance   yplus :  0.42944E+03 0.95450E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63679E+01      60   0.15015E-02   0.20877E-01 
c  VelocityX    0.46298E+04      13   0.71177E-02   0.33194E-03 
c  VelocityY    0.46298E+04      13   0.71177E-02   0.35355E-04 
c  VelocityZ    0.46298E+04      13   0.71177E-02   0.89689E-04 
c  TurbEner     0.59787E+01      13   0.75531E-04   0.10573E-08 
c  Dissip       0.14952E+01      15   0.73169E-03   0.13329E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.04           54517           26777           27271
v  Velocity[x]             0.2929          2.1866         0.90806         0.90983
v  Velocity[y]           -0.38281         0.69359      0.00056259      0.00034536
v  Velocity[z]           -0.41864         0.51049      -0.0012325      -0.0013544
v  TurbEner             0.0010148        0.014908       0.0032864       0.0033459
v  Dissip              9.2047e-05        0.030826      0.00045251      0.00039114
v  TurbVisc                0.1654          11.297          4.7116          5.2728
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              300:        0.97730E-01

===============================================================


 INSTANT    0.301000000E+03   TIME STEP NUMBER             301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000089E+04
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 :  0.23789E+00 0.12256E+01
   Friction velocity        uet   :  0.14227E-01 0.72295E-01
   Friction velocity        uk    :  0.17448E-01 0.38700E-01
   Dimensionless distance   yplus :  0.42896E+03 0.95474E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58031E+01      59   0.14097E-02   0.19031E-01 
c  VelocityX    0.46299E+04      13   0.71102E-02   0.42746E-03 
c  VelocityY    0.46299E+04      13   0.71102E-02   0.27695E-04 
c  VelocityZ    0.46299E+04      13   0.71102E-02   0.40971E-04 
c  TurbEner     0.59783E+01      13   0.13117E-03   0.16073E-08 
c  Dissip       0.15111E+01      16   0.20749E-02   0.48042E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.51           54523           26777           27271
v  Velocity[x]            0.29289          2.0228         0.90806         0.90983
v  Velocity[y]           -0.36736         0.70215      0.00056432      0.00033967
v  Velocity[z]           -0.41969         0.50434      -0.0012479      -0.0013671
v  TurbEner             0.0010173        0.015509       0.0032865       0.0033459
v  Dissip              9.2049e-05        0.032449      0.00045273       0.0003913
v  TurbVisc               0.16506          11.301          4.7116          5.2729
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              301:        0.96559E-01

===============================================================


 INSTANT    0.302000000E+03   TIME STEP NUMBER             302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002352E+04
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 :  0.23820E+00 0.13251E+01
   Friction velocity        uet   :  0.14246E-01 0.78986E-01
   Friction velocity        uk    :  0.17470E-01 0.38746E-01
   Dimensionless distance   yplus :  0.42871E+03 0.95463E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60846E+01      60   0.13190E-02   0.19940E-01 
c  VelocityX    0.46298E+04      12   0.63206E-02   0.34833E-03 
c  VelocityY    0.46298E+04      12   0.63206E-02   0.26175E-04 
c  VelocityZ    0.46298E+04      12   0.63206E-02   0.47864E-04 
c  TurbEner     0.59768E+01      14   0.12838E-03   0.18745E-08 
c  Dissip       0.14793E+01      16   0.20464E-02   0.63277E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.36           54534           26777           27271
v  Velocity[x]            0.29271          2.0925         0.90804         0.90981
v  Velocity[y]           -0.38225         0.69237      0.00054997      0.00032767
v  Velocity[z]           -0.42208         0.51192      -0.0012372      -0.0013573
v  TurbEner             0.0010177         0.01494       0.0032862       0.0033457
v  Dissip              9.1977e-05        0.031153      0.00045247      0.00039112
v  TurbVisc               0.16499          11.336          4.7116          5.2728
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              302:        0.96447E-01

===============================================================


 INSTANT    0.303000000E+03   TIME STEP NUMBER             303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999502E+04
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 :  0.23798E+00 0.12169E+01
   Friction velocity        uet   :  0.14233E-01 0.72538E-01
   Friction velocity        uk    :  0.17473E-01 0.38823E-01
   Dimensionless distance   yplus :  0.42917E+03 0.95400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54002E+01      55   0.11721E-02   0.17706E-01 
c  VelocityX    0.46298E+04      12   0.64564E-02   0.26544E-03 
c  VelocityY    0.46298E+04      12   0.64564E-02   0.23556E-04 
c  VelocityZ    0.46298E+04      12   0.64564E-02   0.46468E-04 
c  TurbEner     0.59770E+01      12   0.67554E-04   0.53187E-09 
c  Dissip       0.14807E+01      14   0.57316E-03   0.42288E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.98           54541           26776           27270
v  Velocity[x]            0.29273          2.1433         0.90806         0.90983
v  Velocity[y]           -0.36607         0.69956      0.00054574      0.00032055
v  Velocity[z]            -0.4221         0.50653      -0.0012583      -0.0013774
v  TurbEner             0.0010153        0.014794       0.0032861       0.0033457
v  Dissip              9.1964e-05        0.030795      0.00045242      0.00039107
v  TurbVisc               0.16529          11.323          4.7116          5.2728
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              303:        0.95690E-01

===============================================================


 INSTANT    0.304000000E+03   TIME STEP NUMBER             304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001730E+04
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 :  0.23817E+00 0.13245E+01
   Friction velocity        uet   :  0.14245E-01 0.78954E-01
   Friction velocity        uk    :  0.17452E-01 0.38866E-01
   Dimensionless distance   yplus :  0.42907E+03 0.95420E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75490E+01      57   0.15083E-02   0.24744E-01 
c  VelocityX    0.46298E+04      12   0.71399E-02   0.36219E-03 
c  VelocityY    0.46298E+04      12   0.71399E-02   0.45457E-04 
c  VelocityZ    0.46298E+04      12   0.71399E-02   0.88728E-04 
c  TurbEner     0.59780E+01      12   0.65131E-04   0.62975E-09 
c  Dissip       0.15041E+01      15   0.66279E-03   0.10765E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.75           54549           26776           27270
v  Velocity[x]            0.29309          2.1894         0.90804         0.90982
v  Velocity[y]           -0.38232         0.69455      0.00056348      0.00034049
v  Velocity[z]           -0.42151         0.51108      -0.0012419      -0.0013644
v  TurbEner             0.0010165        0.014876       0.0032862       0.0033457
v  Dissip              9.1953e-05        0.030939      0.00045255      0.00039115
v  TurbVisc               0.16518          11.324          4.7115          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              304:        0.96142E-01

===============================================================


 INSTANT    0.305000000E+03   TIME STEP NUMBER             305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000464E+04
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 :  0.23796E+00 0.12129E+01
   Friction velocity        uet   :  0.14232E-01 0.72303E-01
   Friction velocity        uk    :  0.17463E-01 0.38831E-01
   Dimensionless distance   yplus :  0.42852E+03 0.95490E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69974E+01      57   0.15235E-02   0.22939E-01 
c  VelocityX    0.46297E+04      13   0.68093E-02   0.41080E-03 
c  VelocityY    0.46297E+04      13   0.68093E-02   0.65217E-04 
c  VelocityZ    0.46297E+04      13   0.68093E-02   0.49801E-04 
c  TurbEner     0.59783E+01      13   0.13461E-03   0.18319E-08 
c  Dissip       0.15088E+01      16   0.19374E-02   0.42001E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.97           54554           26776           27270
v  Velocity[x]            0.29294          2.0083         0.90805         0.90982
v  Velocity[y]           -0.36772         0.70405      0.00055293      0.00032902
v  Velocity[z]           -0.42323         0.50417      -0.0012575      -0.0013744
v  TurbEner             0.0010188        0.015532       0.0032864       0.0033459
v  Dissip              9.2023e-05        0.032441      0.00045272      0.00039128
v  TurbVisc               0.16496          11.355          4.7116          5.2728
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              305:        0.96743E-01

===============================================================


 INSTANT    0.306000000E+03   TIME STEP NUMBER             306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000187E+04
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 :  0.23755E+00 0.13250E+01
   Friction velocity        uet   :  0.14207E-01 0.78978E-01
   Friction velocity        uk    :  0.17482E-01 0.38807E-01
   Dimensionless distance   yplus :  0.42955E+03 0.95476E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64797E+01      54   0.14456E-02   0.21243E-01 
c  VelocityX    0.46298E+04      13   0.70922E-02   0.38331E-03 
c  VelocityY    0.46298E+04      13   0.70922E-02   0.38124E-04 
c  VelocityZ    0.46298E+04      13   0.70922E-02   0.28935E-04 
c  TurbEner     0.59777E+01      13   0.13860E-03   0.19437E-08 
c  Dissip       0.14779E+01      16   0.21968E-02   0.68272E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.16           54544           26776           27270
v  Velocity[x]            0.29252          2.1013         0.90806         0.90984
v  Velocity[y]           -0.38256         0.69167      0.00054992      0.00033248
v  Velocity[z]           -0.42236         0.51163      -0.0012477      -0.0013685
v  TurbEner              0.001015        0.014919       0.0032863       0.0033458
v  Dissip              9.2043e-05        0.030981      0.00045251      0.00039115
v  TurbVisc               0.16556          11.339          4.7116          5.2728
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              306:        0.96017E-01

===============================================================


 INSTANT    0.307000000E+03   TIME STEP NUMBER             307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999920E+04
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 :  0.23786E+00 0.12180E+01
   Friction velocity        uet   :  0.14226E-01 0.72597E-01
   Friction velocity        uk    :  0.17450E-01 0.38735E-01
   Dimensionless distance   yplus :  0.42908E+03 0.95446E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69695E+01      58   0.16486E-02   0.22851E-01 
c  VelocityX    0.46298E+04      12   0.66247E-02   0.38545E-03 
c  VelocityY    0.46298E+04      12   0.66247E-02   0.35992E-04 
c  VelocityZ    0.46298E+04      12   0.66247E-02   0.42988E-04 
c  TurbEner     0.59780E+01      13   0.64635E-04   0.97861E-09 
c  Dissip       0.14839E+01      14   0.30629E-03   0.24543E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.53           54517           26776           27270
v  Velocity[x]            0.29269          2.1396         0.90807         0.90984
v  Velocity[y]           -0.36654         0.70064      0.00055284      0.00033397
v  Velocity[z]           -0.42157         0.50602      -0.0012458      -0.0013634
v  TurbEner             0.0010177        0.014906       0.0032863       0.0033458
v  Dissip              9.2033e-05        0.030862      0.00045249      0.00039114
v  TurbVisc               0.16524          11.346          4.7116          5.2728
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              307:        0.95945E-01

===============================================================


 INSTANT    0.308000000E+03   TIME STEP NUMBER             308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001522E+04
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 :  0.23766E+00 0.13237E+01
   Friction velocity        uet   :  0.14214E-01 0.78895E-01
   Friction velocity        uk    :  0.17473E-01 0.38786E-01
   Dimensionless distance   yplus :  0.42884E+03 0.95399E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.52405E+01      59   0.12253E-02   0.17182E-01 
c  VelocityX    0.46298E+04      12   0.71731E-02   0.27975E-03 
c  VelocityY    0.46298E+04      12   0.71731E-02   0.28534E-04 
c  VelocityZ    0.46298E+04      12   0.71731E-02   0.42456E-04 
c  TurbEner     0.59782E+01      12   0.79268E-04   0.10986E-08 
c  Dissip       0.15043E+01      15   0.78084E-03   0.13455E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.94           54528           26777           27271
v  Velocity[x]            0.29287          2.1765         0.90803         0.90981
v  Velocity[y]           -0.38227          0.6945      0.00054978      0.00033156
v  Velocity[z]           -0.42123         0.51104      -0.0012382      -0.0013591
v  TurbEner             0.0010184        0.015065       0.0032864       0.0033459
v  Dissip              9.2025e-05        0.031238      0.00045262      0.00039121
v  TurbVisc               0.16519          11.383          4.7115          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              308:        0.96189E-01

===============================================================


 INSTANT    0.309000000E+03   TIME STEP NUMBER             309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997637E+04
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 :  0.23785E+00 0.12172E+01
   Friction velocity        uet   :  0.14226E-01 0.72562E-01
   Friction velocity        uk    :  0.17479E-01 0.38849E-01
   Dimensionless distance   yplus :  0.42940E+03 0.95353E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60578E+01      53   0.13350E-02   0.19858E-01 
c  VelocityX    0.46298E+04      13   0.78372E-02   0.37852E-03 
c  VelocityY    0.46298E+04      13   0.78372E-02   0.24219E-04 
c  VelocityZ    0.46298E+04      13   0.78372E-02   0.48257E-04 
c  TurbEner     0.59790E+01      13   0.80426E-04   0.10693E-08 
c  Dissip       0.15311E+01      15   0.83884E-03   0.15104E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.47           54524           26776           27270
v  Velocity[x]            0.29258          2.1992         0.90807         0.90984
v  Velocity[y]           -0.36695         0.70307      0.00055509      0.00033323
v  Velocity[z]           -0.42211         0.50473      -0.0012523      -0.0013716
v  TurbEner             0.0010154        0.015258       0.0032863       0.0033458
v  Dissip              9.2053e-05        0.031691       0.0004528      0.00039133
v  TurbVisc               0.16554           11.36          4.7115          5.2727
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              309:        0.95513E-01

===============================================================


 INSTANT    0.310000000E+03   TIME STEP NUMBER             310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001410E+04
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 :  0.23763E+00 0.13242E+01
   Friction velocity        uet   :  0.14213E-01 0.78936E-01
   Friction velocity        uk    :  0.17454E-01 0.38846E-01
   Dimensionless distance   yplus :  0.42910E+03 0.95319E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.81464E+01      54   0.18154E-02   0.26701E-01 
c  VelocityX    0.46298E+04      12   0.74181E-02   0.49372E-03 
c  VelocityY    0.46298E+04      12   0.74181E-02   0.27534E-04 
c  VelocityZ    0.46298E+04      12   0.74181E-02   0.97942E-04 
c  TurbEner     0.59796E+01      13   0.11995E-03   0.12635E-08 
c  Dissip       0.15488E+01      16   0.20078E-02   0.48536E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.13           54527           26777           27271
v  Velocity[x]            0.29277          2.0418         0.90805         0.90983
v  Velocity[y]           -0.38233         0.69591      0.00056379      0.00034469
v  Velocity[z]           -0.42087         0.51178      -0.0012342      -0.0013524
v  TurbEner             0.0010169        0.015837       0.0032864       0.0033459
v  Dissip              9.2036e-05        0.033292      0.00045306      0.00039151
v  TurbVisc               0.16532          11.362          4.7115          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              310:        0.95714E-01

===============================================================


 INSTANT    0.311000000E+03   TIME STEP NUMBER             311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998626E+04
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 :  0.23736E+00 0.12168E+01
   Friction velocity        uet   :  0.14196E-01 0.72535E-01
   Friction velocity        uk    :  0.17467E-01 0.38807E-01
   Dimensionless distance   yplus :  0.42851E+03 0.95280E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73683E+01      56   0.14685E-02   0.24153E-01 
c  VelocityX    0.46296E+04      12   0.71464E-02   0.59195E-03 
c  VelocityY    0.46296E+04      12   0.71464E-02   0.49273E-04 
c  VelocityZ    0.46296E+04      12   0.71464E-02   0.60522E-04 
c  TurbEner     0.59769E+01      14   0.11226E-03   0.23473E-08 
c  Dissip       0.14996E+01      16   0.15917E-02   0.63403E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.27           54513           26776           27271
v  Velocity[x]            0.29301           1.722         0.90803         0.90981
v  Velocity[y]           -0.36678         0.70167      0.00055148      0.00032944
v  Velocity[z]           -0.42114         0.50573      -0.0012587      -0.0013755
v  TurbEner              0.001019        0.015779       0.0032863       0.0033457
v  Dissip              9.2052e-05        0.033304      0.00045276      0.00039132
v  TurbVisc               0.16507          11.335          4.7115          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              311:        0.95918E-01

===============================================================


 INSTANT    0.312000000E+03   TIME STEP NUMBER             312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000739E+04
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 :  0.23788E+00 0.13260E+01
   Friction velocity        uet   :  0.14228E-01 0.79040E-01
   Friction velocity        uk    :  0.17484E-01 0.38762E-01
   Dimensionless distance   yplus :  0.42944E+03 0.95266E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61712E+01      52   0.14049E-02   0.20242E-01 
c  VelocityX    0.46297E+04      12   0.71644E-02   0.37614E-03 
c  VelocityY    0.46297E+04      12   0.71644E-02   0.36642E-04 
c  VelocityZ    0.46297E+04      12   0.71644E-02   0.30973E-04 
c  TurbEner     0.59728E+01      15   0.40846E-03   0.93231E-08 
c  Dissip       0.13527E+01      18   0.80206E-02   0.46914E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.86           54519           26776           27270
v  Velocity[x]            0.29252          1.8804         0.90804         0.90982
v  Velocity[y]           -0.38281           0.693      0.00055272      0.00033424
v  Velocity[z]           -0.42071         0.51052      -0.0012523      -0.0013715
v  TurbEner             0.0010152        0.013577        0.003286       0.0033455
v  Dissip              9.2137e-05        0.027698      0.00045206      0.00039077
v  TurbVisc               0.16561          11.331          4.7115          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              312:        0.95415E-01

===============================================================


 INSTANT    0.313000000E+03   TIME STEP NUMBER             313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000683E+04
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 :  0.23785E+00 0.12159E+01
   Friction velocity        uet   :  0.14225E-01 0.72479E-01
   Friction velocity        uk    :  0.17452E-01 0.38718E-01
   Dimensionless distance   yplus :  0.42901E+03 0.95282E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64864E+01      54   0.14907E-02   0.21257E-01 
c  VelocityX    0.46297E+04      12   0.74547E-02   0.40696E-03 
c  VelocityY    0.46297E+04      12   0.74547E-02   0.25632E-04 
c  VelocityZ    0.46297E+04      12   0.74547E-02   0.40783E-04 
c  TurbEner     0.59712E+01      14   0.15735E-03   0.25495E-08 
c  Dissip       0.12979E+01      18   0.36382E-02   0.12698E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.49           54496           26776           27270
v  Velocity[x]             0.2928          1.9924         0.90806         0.90983
v  Velocity[y]           -0.36734         0.70127      0.00055592      0.00033447
v  Velocity[z]           -0.42042          0.5043      -0.0012533      -0.0013711
v  TurbEner             0.0010177        0.012862       0.0032857       0.0033452
v  Dissip              9.2174e-05        0.025383      0.00045139      0.00039029
v  TurbVisc               0.16529          11.357          4.7116          5.2728
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              313:        0.95644E-01

===============================================================


 INSTANT    0.314000000E+03   TIME STEP NUMBER             314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001436E+04
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 :  0.23772E+00 0.13236E+01
   Friction velocity        uet   :  0.14217E-01 0.78900E-01
   Friction velocity        uk    :  0.17473E-01 0.38780E-01
   Dimensionless distance   yplus :  0.42882E+03 0.95236E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64860E+01      59   0.12947E-02   0.21266E-01 
c  VelocityX    0.46298E+04      12   0.66664E-02   0.36615E-03 
c  VelocityY    0.46298E+04      12   0.66664E-02   0.26081E-04 
c  VelocityZ    0.46298E+04      12   0.66664E-02   0.77265E-04 
c  TurbEner     0.59703E+01      13   0.10065E-03   0.17630E-08 
c  Dissip       0.12667E+01      18   0.23071E-02   0.84166E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.78           54509           26776           27270
v  Velocity[x]            0.29307          2.0749         0.90804         0.90982
v  Velocity[y]           -0.38214         0.69379      0.00056721      0.00034581
v  Velocity[z]           -0.42154         0.51184       -0.001243      -0.0013641
v  TurbEner              0.001018        0.012769       0.0032853       0.0033449
v  Dissip              9.2142e-05         0.02443      0.00045067      0.00038978
v  TurbVisc               0.16523          11.335          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              314:        0.96128E-01

===============================================================


 INSTANT    0.315000000E+03   TIME STEP NUMBER             315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000744E+04
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 :  0.23786E+00 0.12162E+01
   Friction velocity        uet   :  0.14226E-01 0.72502E-01
   Friction velocity        uk    :  0.17475E-01 0.38808E-01
   Dimensionless distance   yplus :  0.42935E+03 0.95200E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67829E+01      57   0.14763E-02   0.22242E-01 
c  VelocityX    0.46298E+04      12   0.70079E-02   0.37750E-03 
c  VelocityY    0.46298E+04      12   0.70079E-02   0.40131E-04 
c  VelocityZ    0.46298E+04      12   0.70079E-02   0.46364E-04 
c  TurbEner     0.59703E+01      13   0.70844E-04   0.10601E-08 
c  Dissip       0.12527E+01      17   0.10468E-02   0.22281E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.21           54514           26775           27270
v  Velocity[x]            0.29237           2.116         0.90806         0.90984
v  Velocity[y]           -0.36605         0.70002      0.00055529      0.00033325
v  Velocity[z]           -0.42266         0.50657      -0.0012591      -0.0013792
v  TurbEner             0.0010147        0.012961       0.0032849       0.0033446
v  Dissip              9.2109e-05        0.024131      0.00045005      0.00038935
v  TurbVisc               0.16553          11.347          4.7117          5.2729
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              315:        0.95823E-01

===============================================================


 INSTANT    0.316000000E+03   TIME STEP NUMBER             316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001674E+04
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 :  0.23742E+00 0.13251E+01
   Friction velocity        uet   :  0.14198E-01 0.78987E-01
   Friction velocity        uk    :  0.17447E-01 0.38799E-01
   Dimensionless distance   yplus :  0.42910E+03 0.95210E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70315E+01      58   0.14762E-02   0.23056E-01 
c  VelocityX    0.46299E+04      12   0.71150E-02   0.37365E-03 
c  VelocityY    0.46299E+04      12   0.71150E-02   0.45672E-04 
c  VelocityZ    0.46299E+04      12   0.71150E-02   0.34940E-04 
c  TurbEner     0.59711E+01      13   0.85735E-04   0.12158E-08 
c  Dissip       0.12576E+01      16   0.52375E-03   0.65060E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.89           54503           26776           27270
v  Velocity[x]            0.29286          2.1652         0.90807         0.90985
v  Velocity[y]           -0.38227         0.69342      0.00056201      0.00034212
v  Velocity[z]           -0.41998         0.51109      -0.0012301       -0.001349
v  TurbEner             0.0010153        0.013292       0.0032847       0.0033445
v  Dissip              9.2112e-05        0.024361      0.00044962      0.00038905
v  TurbVisc               0.16527          11.328          4.7117          5.2729
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              316:        0.96161E-01

===============================================================


 INSTANT    0.317000000E+03   TIME STEP NUMBER             317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998403E+04
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 :  0.23758E+00 0.12136E+01
   Friction velocity        uet   :  0.14208E-01 0.72297E-01
   Friction velocity        uk    :  0.17453E-01 0.38730E-01
   Dimensionless distance   yplus :  0.42838E+03 0.95208E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63483E+01      65   0.13844E-02   0.20820E-01 
c  VelocityX    0.46297E+04      13   0.69553E-02   0.40795E-03 
c  VelocityY    0.46297E+04      13   0.69553E-02   0.38177E-04 
c  VelocityZ    0.46297E+04      13   0.69553E-02   0.43836E-04 
c  TurbEner     0.59715E+01      14   0.14691E-03   0.24576E-08 
c  Dissip       0.12673E+01      16   0.19259E-02   0.36486E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.12           54507           26776           27270
v  Velocity[x]            0.29312          1.9973         0.90805         0.90983
v  Velocity[y]           -0.36769         0.70205      0.00055319        0.000329
v  Velocity[z]           -0.41987         0.50418       -0.001253      -0.0013705
v  TurbEner             0.0010167        0.014084       0.0032847       0.0033444
v  Dissip              9.2125e-05        0.025773      0.00044936      0.00038887
v  TurbVisc                 0.165          11.313          4.7118           5.273
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              317:        0.98612E-01

===============================================================


 INSTANT    0.318000000E+03   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000066E+04
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 :  0.23771E+00 0.13246E+01
   Friction velocity        uet   :  0.14216E-01 0.78958E-01
   Friction velocity        uk    :  0.17465E-01 0.38755E-01
   Dimensionless distance   yplus :  0.42922E+03 0.95257E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61561E+01      56   0.14564E-02   0.20188E-01 
c  VelocityX    0.46299E+04      12   0.70539E-02   0.34210E-03 
c  VelocityY    0.46299E+04      12   0.70539E-02   0.36992E-04 
c  VelocityZ    0.46299E+04      12   0.70539E-02   0.10567E-03 
c  TurbEner     0.59713E+01      13   0.84475E-04   0.13085E-08 
c  Dissip       0.12485E+01      16   0.15508E-02   0.35913E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.19           54517           26776           27270
v  Velocity[x]            0.29251          2.0824         0.90803         0.90981
v  Velocity[y]           -0.38249         0.69284      0.00055631      0.00033679
v  Velocity[z]           -0.41968          0.5117      -0.0012356      -0.0013594
v  TurbEner             0.0010122        0.013805       0.0032845       0.0033443
v  Dissip              9.2096e-05        0.024895      0.00044894      0.00038857
v  TurbVisc               0.16552          11.337           4.712          5.2731
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              318:        0.95908E-01

===============================================================


 INSTANT    0.319000000E+03   TIME STEP NUMBER             319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999621E+04
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 :  0.23763E+00 0.12151E+01
   Friction velocity        uet   :  0.14212E-01 0.72431E-01
   Friction velocity        uk    :  0.17426E-01 0.38705E-01
   Dimensionless distance   yplus :  0.42859E+03 0.95343E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69610E+01      63   0.15675E-02   0.22821E-01 
c  VelocityX    0.46298E+04      12   0.70417E-02   0.44563E-03 
c  VelocityY    0.46298E+04      12   0.70417E-02   0.36017E-04 
c  VelocityZ    0.46298E+04      12   0.70417E-02   0.54377E-04 
c  TurbEner     0.59719E+01      13   0.73589E-04   0.10936E-08 
c  Dissip       0.12563E+01      15   0.44151E-03   0.51196E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.69           54506           26776           27270
v  Velocity[x]            0.29253          2.1336         0.90807         0.90984
v  Velocity[y]           -0.36615         0.70004      0.00055871      0.00033609
v  Velocity[z]           -0.41923         0.50641        -0.00124      -0.0013574
v  TurbEner             0.0010141        0.013926       0.0032845       0.0033443
v  Dissip              9.2049e-05        0.024886      0.00044875      0.00038844
v  TurbVisc               0.16515          11.381          4.7122          5.2733
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              319:        0.96582E-01

===============================================================


 INSTANT    0.320000000E+03   TIME STEP NUMBER             320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999590E+04
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 :  0.23756E+00 0.13242E+01
   Friction velocity        uet   :  0.14209E-01 0.78929E-01
   Friction velocity        uk    :  0.17442E-01 0.38733E-01
   Dimensionless distance   yplus :  0.42818E+03 0.95315E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60469E+01      65   0.12213E-02   0.19825E-01 
c  VelocityX    0.46300E+04      12   0.67825E-02   0.36499E-03 
c  VelocityY    0.46300E+04      12   0.67825E-02   0.29332E-04 
c  VelocityZ    0.46300E+04      12   0.67825E-02   0.33642E-04 
c  TurbEner     0.59730E+01      13   0.97128E-04   0.17167E-08 
c  Dissip       0.12798E+01      16   0.10422E-02   0.21974E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.53           54510           26777           27271
v  Velocity[x]            0.29299          2.1727         0.90804         0.90982
v  Velocity[y]           -0.38239         0.69142      0.00055026      0.00033069
v  Velocity[z]           -0.42151         0.51095      -0.0012453      -0.0013662
v  TurbEner             0.0010137         0.01422       0.0032847       0.0033444
v  Dissip              9.2026e-05        0.025377       0.0004488      0.00038848
v  TurbVisc               0.16505          11.366          4.7124          5.2735
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              320:        0.98209E-01

===============================================================


 INSTANT    0.321000000E+03   TIME STEP NUMBER             321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998368E+04
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 :  0.23747E+00 0.12154E+01
   Friction velocity        uet   :  0.14204E-01 0.72449E-01
   Friction velocity        uk    :  0.17439E-01 0.38779E-01
   Dimensionless distance   yplus :  0.42846E+03 0.95284E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66506E+01      59   0.15185E-02   0.21813E-01 
c  VelocityX    0.46300E+04      12   0.66355E-02   0.38115E-03 
c  VelocityY    0.46300E+04      12   0.66355E-02   0.36402E-04 
c  VelocityZ    0.46300E+04      12   0.66355E-02   0.41483E-04 
c  TurbEner     0.59740E+01      14   0.13194E-03   0.20182E-08 
c  Dissip       0.13005E+01      17   0.20999E-02   0.52344E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.42           54513           26777           27271
v  Velocity[x]            0.29291          2.0007         0.90807         0.90984
v  Velocity[y]           -0.36792         0.70022       0.0005468      0.00032716
v  Velocity[z]           -0.41925         0.50399      -0.0012562      -0.0013751
v  TurbEner             0.0010111        0.014953       0.0032848       0.0033445
v  Dissip              9.2054e-05        0.026959      0.00044891      0.00038856
v  TurbVisc               0.16532          11.373          4.7127          5.2738
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              321:        0.97304E-01

===============================================================


 INSTANT    0.322000000E+03   TIME STEP NUMBER             322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000194E+04
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 :  0.23750E+00 0.13232E+01
   Friction velocity        uet   :  0.14207E-01 0.78881E-01
   Friction velocity        uk    :  0.17416E-01 0.38725E-01
   Dimensionless distance   yplus :  0.42828E+03 0.95344E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66715E+01      61   0.15529E-02   0.21883E-01 
c  VelocityX    0.46300E+04      12   0.66128E-02   0.33875E-03 
c  VelocityY    0.46300E+04      12   0.66128E-02   0.54222E-04 
c  VelocityZ    0.46300E+04      12   0.66128E-02   0.12483E-03 
c  TurbEner     0.59736E+01      14   0.97296E-04   0.17334E-08 
c  Dissip       0.12883E+01      16   0.13560E-02   0.30757E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.61           54520           26778           27272
v  Velocity[x]            0.29261          2.0868         0.90804         0.90981
v  Velocity[y]           -0.38299         0.69325      0.00056424      0.00034486
v  Velocity[z]           -0.41718         0.51122      -0.0012253      -0.0013493
v  TurbEner             0.0010127        0.014561       0.0032848       0.0033445
v  Dissip              9.2072e-05        0.026168      0.00044877      0.00038847
v  TurbVisc               0.16525          11.349          4.7129          5.2739
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              322:        0.96686E-01

===============================================================


 INSTANT    0.323000000E+03   TIME STEP NUMBER             323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998150E+04
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 :  0.23734E+00 0.12152E+01
   Friction velocity        uet   :  0.14199E-01 0.72445E-01
   Friction velocity        uk    :  0.17430E-01 0.38769E-01
   Dimensionless distance   yplus :  0.42772E+03 0.95339E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61799E+01      63   0.13575E-02   0.20266E-01 
c  VelocityX    0.46300E+04      12   0.70197E-02   0.36583E-03 
c  VelocityY    0.46300E+04      12   0.70197E-02   0.33735E-04 
c  VelocityZ    0.46300E+04      12   0.70197E-02   0.55670E-04 
c  TurbEner     0.59737E+01      13   0.63978E-04   0.93960E-09 
c  Dissip       0.13012E+01      15   0.53866E-03   0.78359E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.58           54514           26778           27272
v  Velocity[x]            0.29301          2.1351         0.90806         0.90984
v  Velocity[y]           -0.36802         0.70014      0.00055852      0.00033577
v  Velocity[z]           -0.41956         0.50708      -0.0012437      -0.0013637
v  TurbEner             0.0010154        0.014585       0.0032849       0.0033446
v  Dissip              9.2109e-05        0.026232      0.00044885      0.00038851
v  TurbVisc               0.16512          11.348          4.7131          5.2741
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              323:        0.97758E-01

===============================================================


 INSTANT    0.324000000E+03   TIME STEP NUMBER             324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999494E+04
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 :  0.23762E+00 0.13248E+01
   Friction velocity        uet   :  0.14217E-01 0.78971E-01
   Friction velocity        uk    :  0.17453E-01 0.38819E-01
   Dimensionless distance   yplus :  0.42878E+03 0.95356E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63702E+01      53   0.13833E-02   0.20885E-01 
c  VelocityX    0.46302E+04      13   0.76649E-02   0.39698E-03 
c  VelocityY    0.46302E+04      13   0.76649E-02   0.22795E-04 
c  VelocityZ    0.46302E+04      13   0.76649E-02   0.32442E-04 
c  TurbEner     0.59754E+01      13   0.81722E-04   0.11287E-08 
c  Dissip       0.13283E+01      16   0.10935E-02   0.26188E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.28           54518           26778           27272
v  Velocity[x]             0.2926          2.1741         0.90805         0.90983
v  Velocity[y]           -0.38277         0.69444      0.00055043      0.00033052
v  Velocity[z]           -0.41903         0.51382      -0.0012396      -0.0013625
v  TurbEner             0.0010125        0.014763       0.0032852       0.0033447
v  Dissip              9.2141e-05         0.02674      0.00044912      0.00038868
v  TurbVisc               0.16583          11.324          4.7134          5.2744
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              324:        0.95902E-01

===============================================================


 INSTANT    0.325000000E+03   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998997E+04
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 :  0.23831E+00 0.12152E+01
   Friction velocity        uet   :  0.14259E-01 0.72293E-01
   Friction velocity        uk    :  0.17428E-01 0.38758E-01
   Dimensionless distance   yplus :  0.42845E+03 0.95411E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67891E+01      57   0.15664E-02   0.22270E-01 
c  VelocityX    0.46301E+04      12   0.72327E-02   0.44676E-03 
c  VelocityY    0.46301E+04      12   0.72327E-02   0.47681E-04 
c  VelocityZ    0.46301E+04      12   0.72327E-02   0.41594E-04 
c  TurbEner     0.59761E+01      14   0.12191E-03   0.18343E-08 
c  Dissip       0.13510E+01      16   0.20625E-02   0.52382E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.5           54505           26778           27272
v  Velocity[x]            0.29279          2.0035         0.90806         0.90984
v  Velocity[y]            -0.3666         0.70272      0.00056051      0.00033962
v  Velocity[z]           -0.41984         0.50786      -0.0012498      -0.0013693
v  TurbEner             0.0010163        0.015407       0.0032855       0.0033449
v  Dissip               9.213e-05        0.028344      0.00044945      0.00038891
v  TurbVisc               0.16568          11.321          4.7137          5.2746
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              325:        0.95875E-01

===============================================================


 INSTANT    0.326000000E+03   TIME STEP NUMBER             326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000755E+04
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 :  0.23765E+00 0.13255E+01
   Friction velocity        uet   :  0.14220E-01 0.79012E-01
   Friction velocity        uk    :  0.17462E-01 0.38692E-01
   Dimensionless distance   yplus :  0.42841E+03 0.95423E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65921E+01      65   0.13272E-02   0.21617E-01 
c  VelocityX    0.46301E+04      12   0.63371E-02   0.37068E-03 
c  VelocityY    0.46301E+04      12   0.63371E-02   0.25782E-04 
c  VelocityZ    0.46301E+04      12   0.63371E-02   0.97659E-04 
c  TurbEner     0.59749E+01      14   0.11224E-03   0.19928E-08 
c  Dissip       0.13330E+01      16   0.14946E-02   0.38809E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.69           54515           26778           27272
v  Velocity[x]            0.29304           2.086         0.90805         0.90983
v  Velocity[y]           -0.38273          0.6924      0.00055655      0.00033407
v  Velocity[z]           -0.42128         0.51203      -0.0012393      -0.0013639
v  TurbEner             0.0010184        0.014902       0.0032857        0.003345
v  Dissip              9.2084e-05        0.027459      0.00044943      0.00038889
v  TurbVisc               0.16584          11.348          4.7139          5.2748
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              326:        0.96865E-01

===============================================================


 INSTANT    0.327000000E+03   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000764E+04
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 :  0.23758E+00 0.12176E+01
   Friction velocity        uet   :  0.14218E-01 0.72580E-01
   Friction velocity        uk    :  0.17479E-01 0.38781E-01
   Dimensionless distance   yplus :  0.42922E+03 0.95464E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57768E+01      58   0.13476E-02   0.18944E-01 
c  VelocityX    0.46303E+04      12   0.68155E-02   0.32899E-03 
c  VelocityY    0.46303E+04      12   0.68155E-02   0.27057E-04 
c  VelocityZ    0.46303E+04      12   0.68155E-02   0.46518E-04 
c  TurbEner     0.59755E+01      12   0.57693E-04   0.68451E-09 
c  Dissip       0.13469E+01      15   0.45838E-03   0.57009E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.49           54510           26777           27271
v  Velocity[x]            0.29272          2.1365         0.90808         0.90985
v  Velocity[y]           -0.36842         0.69988      0.00055224      0.00033079
v  Velocity[z]           -0.42031          0.5046      -0.0012517      -0.0013704
v  TurbEner             0.0010177        0.014848       0.0032858       0.0033451
v  Dissip              9.2024e-05        0.027517      0.00044959      0.00038899
v  TurbVisc               0.16643           11.33          4.7141           5.275
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              327:        0.96083E-01

===============================================================


 INSTANT    0.328000000E+03   TIME STEP NUMBER             328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002082E+04
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 :  0.23806E+00 0.13238E+01
   Friction velocity        uet   :  0.14247E-01 0.78905E-01
   Friction velocity        uk    :  0.17473E-01 0.38844E-01
   Dimensionless distance   yplus :  0.42938E+03 0.95511E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61880E+01      58   0.14808E-02   0.20295E-01 
c  VelocityX    0.46303E+04      12   0.72721E-02   0.34748E-03 
c  VelocityY    0.46303E+04      12   0.72721E-02   0.23725E-04 
c  VelocityZ    0.46303E+04      12   0.72721E-02   0.33251E-04 
c  TurbEner     0.59767E+01      13   0.84976E-04   0.12066E-08 
c  Dissip       0.13752E+01      16   0.10298E-02   0.23249E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.41           54506           26778           27272
v  Velocity[x]            0.29228          2.1748         0.90807         0.90985
v  Velocity[y]           -0.38277         0.69297      0.00055876      0.00034014
v  Velocity[z]           -0.42063         0.51218       -0.001235      -0.0013558
v  TurbEner             0.0010216         0.01497       0.0032862       0.0033454
v  Dissip              9.2046e-05         0.02803      0.00044993      0.00038921
v  TurbVisc               0.16658          11.336          4.7143          5.2753
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              328:        0.96442E-01

===============================================================


 INSTANT    0.329000000E+03   TIME STEP NUMBER             329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999498E+04
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 :  0.23746E+00 0.12160E+01
   Friction velocity        uet   :  0.14212E-01 0.72482E-01
   Friction velocity        uk    :  0.17506E-01 0.38875E-01
   Dimensionless distance   yplus :  0.42923E+03 0.95481E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63551E+01      56   0.13687E-02   0.20841E-01 
c  VelocityX    0.46303E+04      12   0.68131E-02   0.41523E-03 
c  VelocityY    0.46303E+04      12   0.68131E-02   0.38843E-04 
c  VelocityZ    0.46303E+04      12   0.68131E-02   0.34161E-04 
c  TurbEner     0.59767E+01      13   0.11170E-03   0.15523E-08 
c  Dissip       0.13961E+01      16   0.21042E-02   0.53312E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -178.3           54502           26777           27272
v  Velocity[x]            0.29311          2.0044         0.90806         0.90984
v  Velocity[y]           -0.36666         0.70204      0.00054893      0.00032848
v  Velocity[z]           -0.42084         0.50634       -0.001254      -0.0013686
v  TurbEner             0.0010266        0.015555       0.0032864       0.0033455
v  Dissip              9.2001e-05        0.029683      0.00045023      0.00038941
v  TurbVisc               0.16671          11.375          4.7146          5.2755
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              329:        0.95808E-01

===============================================================


 INSTANT    0.330000000E+03   TIME STEP NUMBER             330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001525E+04
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 :  0.23755E+00 0.13234E+01
   Friction velocity        uet   :  0.14218E-01 0.78878E-01
   Friction velocity        uk    :  0.17550E-01 0.38861E-01
   Dimensionless distance   yplus :  0.43076E+03 0.95531E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60672E+01      59   0.13644E-02   0.19904E-01 
c  VelocityX    0.46303E+04      12   0.64481E-02   0.27375E-03 
c  VelocityY    0.46303E+04      12   0.64481E-02   0.40215E-04 
c  VelocityZ    0.46303E+04      12   0.64481E-02   0.56429E-04 
c  TurbEner     0.59761E+01      14   0.12339E-03   0.19748E-08 
c  Dissip       0.13790E+01      16   0.15607E-02   0.40544E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.95           54523           26778           27272
v  Velocity[x]            0.29288          2.0838         0.90804         0.90982
v  Velocity[y]           -0.38247         0.69437      0.00055069      0.00033156
v  Velocity[z]           -0.42063         0.51118      -0.0012474      -0.0013683
v  TurbEner             0.0010261        0.015008       0.0032864       0.0033455
v  Dissip              9.1991e-05        0.028728      0.00045017      0.00038935
v  TurbVisc               0.16775          11.354          4.7148          5.2757
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              330:        0.96198E-01

===============================================================


 INSTANT    0.331000000E+03   TIME STEP NUMBER             331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999761E+04
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 :  0.23786E+00 0.12168E+01
   Friction velocity        uet   :  0.14237E-01 0.72536E-01
   Friction velocity        uk    :  0.17545E-01 0.38769E-01
   Dimensionless distance   yplus :  0.43093E+03 0.95560E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60209E+01      54   0.11869E-02   0.19746E-01 
c  VelocityX    0.46303E+04      13   0.69543E-02   0.32769E-03 
c  VelocityY    0.46303E+04      13   0.69543E-02   0.29705E-04 
c  VelocityZ    0.46303E+04      13   0.69543E-02   0.39308E-04 
c  TurbEner     0.59763E+01      12   0.62389E-04   0.60110E-09 
c  Dissip       0.13883E+01      14   0.42866E-03   0.42844E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.67           54538           26777           27272
v  Velocity[x]            0.29264          2.1316         0.90806         0.90984
v  Velocity[y]            -0.3677         0.70062       0.0005487      0.00032524
v  Velocity[z]           -0.42142         0.50455      -0.0012543      -0.0013741
v  TurbEner             0.0010326        0.014888       0.0032865       0.0033456
v  Dissip              9.1976e-05         0.02862      0.00045029      0.00038942
v  TurbVisc               0.16792          11.356          4.7149          5.2759
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              331:        0.96010E-01

===============================================================


 INSTANT    0.332000000E+03   TIME STEP NUMBER             332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000484E+04
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 :  0.23749E+00 0.13253E+01
   Friction velocity        uet   :  0.14215E-01 0.78993E-01
   Friction velocity        uk    :  0.17601E-01 0.38797E-01
   Dimensionless distance   yplus :  0.43139E+03 0.95530E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58749E+01      55   0.12102E-02   0.19262E-01 
c  VelocityX    0.46303E+04      12   0.70754E-02   0.35100E-03 
c  VelocityY    0.46303E+04      12   0.70754E-02   0.25206E-04 
c  VelocityZ    0.46303E+04      12   0.70754E-02   0.31108E-04 
c  TurbEner     0.59777E+01      13   0.68484E-04   0.78121E-09 
c  Dissip       0.14172E+01      15   0.85797E-03   0.17066E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.83           54549           26778           27272
v  Velocity[x]            0.29282          2.1797         0.90807         0.90984
v  Velocity[y]           -0.38225         0.69402      0.00053849      0.00031807
v  Velocity[z]           -0.41837         0.51209      -0.0012398      -0.0013596
v  TurbEner              0.001037         0.01497       0.0032867       0.0033458
v  Dissip              9.2004e-05        0.028982      0.00045058      0.00038962
v  TurbVisc               0.16838          11.332          4.7151          5.2761
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              332:        0.95786E-01

===============================================================


 INSTANT    0.333000000E+03   TIME STEP NUMBER             333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999647E+04
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 :  0.23766E+00 0.12138E+01
   Friction velocity        uet   :  0.14226E-01 0.72302E-01
   Friction velocity        uk    :  0.17638E-01 0.38850E-01
   Dimensionless distance   yplus :  0.43266E+03 0.95497E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70214E+01      54   0.16162E-02   0.23025E-01 
c  VelocityX    0.46304E+04      12   0.77022E-02   0.30592E-03 
c  VelocityY    0.46304E+04      12   0.77022E-02   0.32433E-04 
c  VelocityZ    0.46304E+04      12   0.77022E-02   0.96176E-04 
c  TurbEner     0.59789E+01      13   0.76932E-04   0.97237E-09 
c  Dissip       0.14473E+01      16   0.10471E-02   0.21321E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.13           54541           26777           27272
v  Velocity[x]            0.29294          2.2011         0.90807         0.90985
v  Velocity[y]            -0.3661          0.7025      0.00055532      0.00033441
v  Velocity[z]           -0.42067         0.50658      -0.0012385      -0.0013595
v  TurbEner             0.0010381        0.015211       0.0032869       0.0033459
v  Dissip              9.2022e-05        0.029629      0.00045092      0.00038985
v  TurbVisc               0.16922          11.327          4.7153          5.2763
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              333:        0.95570E-01

===============================================================


 INSTANT    0.334000000E+03   TIME STEP NUMBER             334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000662E+04
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 :  0.23763E+00 0.13246E+01
   Friction velocity        uet   :  0.14224E-01 0.78957E-01
   Friction velocity        uk    :  0.17647E-01 0.38895E-01
   Dimensionless distance   yplus :  0.43328E+03 0.95528E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.77449E+01      64   0.18108E-02   0.25412E-01 
c  VelocityX    0.46302E+04      12   0.74517E-02   0.90420E-03 
c  VelocityY    0.46302E+04      12   0.74517E-02   0.52095E-04 
c  VelocityZ    0.46302E+04      12   0.74517E-02   0.79584E-04 
c  TurbEner     0.59791E+01      14   0.22536E-03   0.33744E-08 
c  Dissip       0.14539E+01      17   0.40792E-02   0.16657E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.15           54518           26778           27273
v  Velocity[x]            0.29265          1.6152         0.90806         0.90983
v  Velocity[y]           -0.38238         0.69342      0.00054959      0.00033243
v  Velocity[z]           -0.42128         0.51105      -0.0012455      -0.0013657
v  TurbEner             0.0010429        0.016476       0.0032873       0.0033463
v  Dissip              9.2021e-05         0.03297      0.00045134      0.00039019
v  TurbVisc               0.16955          11.353          4.7154          5.2764
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              334:        0.98217E-01

===============================================================


 INSTANT    0.335000000E+03   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998761E+04
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 :  0.23751E+00 0.12378E+01
   Friction velocity        uet   :  0.14217E-01 0.72466E-01
   Friction velocity        uk    :  0.17688E-01 0.38882E-01
   Dimensionless distance   yplus :  0.43344E+03 0.95545E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58098E+01      53   0.12047E-02   0.19049E-01 
c  VelocityX    0.46302E+04      13   0.70063E-02   0.42706E-03 
c  VelocityY    0.46302E+04      13   0.70063E-02   0.33675E-04 
c  VelocityZ    0.46302E+04      13   0.70063E-02   0.39720E-04 
c  TurbEner     0.59720E+01      16   0.52894E-03   0.17641E-07 
c  Dissip       0.12724E+01      19   0.10356E-01   0.83127E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.65           54526           26778           27272
v  Velocity[x]            0.29285          1.8053         0.90804         0.90981
v  Velocity[y]            -0.3681         0.69961      0.00055179      0.00033078
v  Velocity[z]           -0.42045         0.50393      -0.0012441      -0.0013638
v  TurbEner             0.0010484        0.013455        0.003287        0.003346
v  Dissip               9.201e-05        0.025888       0.0004505      0.00038957
v  TurbVisc               0.16971          11.332          4.7155          5.2765
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              335:        0.96697E-01

===============================================================


 INSTANT    0.336000000E+03   TIME STEP NUMBER             336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001000E+04
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 :  0.23786E+00 0.13242E+01
   Friction velocity        uet   :  0.14238E-01 0.78931E-01
   Friction velocity        uk    :  0.17735E-01 0.38851E-01
   Dimensionless distance   yplus :  0.43511E+03 0.95571E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54039E+01      56   0.11572E-02   0.17727E-01 
c  VelocityX    0.46303E+04      12   0.60918E-02   0.35163E-03 
c  VelocityY    0.46303E+04      12   0.60918E-02   0.20372E-04 
c  VelocityZ    0.46303E+04      12   0.60918E-02   0.34421E-04 
c  TurbEner     0.59702E+01      14   0.20025E-03   0.44348E-08 
c  Dissip       0.12088E+01      19   0.44991E-02   0.20734E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.82           54536           26779           27273
v  Velocity[x]            0.29262          1.9512         0.90805         0.90982
v  Velocity[y]           -0.38252         0.69138      0.00054001       0.0003233
v  Velocity[z]           -0.42113         0.51167      -0.0012446       -0.001365
v  TurbEner             0.0010465        0.012488       0.0032866       0.0033458
v  Dissip                 9.2e-05        0.023214      0.00044976      0.00038905
v  TurbVisc               0.17063          11.342          4.7156          5.2767
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              336:        0.96190E-01

===============================================================


 INSTANT    0.337000000E+03   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998705E+04
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 :  0.23779E+00 0.12151E+01
   Friction velocity        uet   :  0.14234E-01 0.72435E-01
   Friction velocity        uk    :  0.17719E-01 0.38760E-01
   Dimensionless distance   yplus :  0.43510E+03 0.95557E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55203E+01      53   0.12399E-02   0.18105E-01 
c  VelocityX    0.46303E+04      12   0.70958E-02   0.31007E-03 
c  VelocityY    0.46303E+04      12   0.70958E-02   0.22805E-04 
c  VelocityZ    0.46303E+04      12   0.70958E-02   0.29396E-04 
c  TurbEner     0.59697E+01      13   0.90207E-04   0.14231E-08 
c  Dissip       0.11796E+01      18   0.22156E-02   0.65718E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.91           54545           26778           27272
v  Velocity[x]             0.2928          2.0383         0.90806         0.90983
v  Velocity[y]           -0.36669         0.70051      0.00054203      0.00031912
v  Velocity[z]           -0.42085         0.50584      -0.0012496      -0.0013687
v  TurbEner             0.0010509          0.0123       0.0032863       0.0033456
v  Dissip              9.1988e-05        0.022091      0.00044909      0.00038859
v  TurbVisc               0.17047          11.324          4.7157          5.2768
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              337:        0.95587E-01

===============================================================


 INSTANT    0.338000000E+03   TIME STEP NUMBER             338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000116E+04
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 :  0.23770E+00 0.13224E+01
   Friction velocity        uet   :  0.14228E-01 0.78832E-01
   Friction velocity        uk    :  0.17756E-01 0.38811E-01
   Dimensionless distance   yplus :  0.43524E+03 0.95547E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57725E+01      55   0.12176E-02   0.18930E-01 
c  VelocityX    0.46303E+04      12   0.73950E-02   0.32484E-03 
c  VelocityY    0.46303E+04      12   0.73950E-02   0.23363E-04 
c  VelocityZ    0.46303E+04      12   0.73950E-02   0.61308E-04 
c  TurbEner     0.59703E+01      13   0.74028E-04   0.81261E-09 
c  Dissip       0.11681E+01      17   0.10646E-02   0.23526E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.46           54553           26778           27273
v  Velocity[x]            0.29284          2.0958         0.90806         0.90983
v  Velocity[y]           -0.38246         0.69338      0.00055206      0.00033177
v  Velocity[z]           -0.42008         0.51088      -0.0012482       -0.001369
v  TurbEner             0.0010525        0.012543       0.0032863       0.0033456
v  Dissip              9.2033e-05        0.021845      0.00044857      0.00038823
v  TurbVisc               0.17053          11.324          4.7159           5.277
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              338:        0.94423E-01

===============================================================


 INSTANT    0.339000000E+03   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999128E+04
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 :  0.23738E+00 0.12158E+01
   Friction velocity        uet   :  0.14209E-01 0.72486E-01
   Friction velocity        uk    :  0.17769E-01 0.38880E-01
   Dimensionless distance   yplus :  0.43607E+03 0.95537E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53253E+01      53   0.11584E-02   0.17466E-01 
c  VelocityX    0.46303E+04      12   0.68113E-02   0.29116E-03 
c  VelocityY    0.46303E+04      12   0.68113E-02   0.57596E-04 
c  VelocityZ    0.46303E+04      12   0.68113E-02   0.97743E-04 
c  TurbEner     0.59714E+01      13   0.91850E-04   0.12945E-08 
c  Dissip       0.11715E+01      16   0.46998E-03   0.67886E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.4           54557           26778           27272
v  Velocity[x]            0.29267          2.1387         0.90806         0.90984
v  Velocity[y]           -0.36748         0.69958      0.00055785      0.00033241
v  Velocity[z]           -0.42169         0.50442      -0.0012427      -0.0013642
v  TurbEner             0.0010505        0.012927       0.0032862       0.0033456
v  Dissip              9.2056e-05        0.021933      0.00044819      0.00038797
v  TurbVisc               0.17093          11.357          4.7162          5.2773
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              339:        0.93814E-01

===============================================================


 INSTANT    0.340000000E+03   TIME STEP NUMBER             340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000632E+04
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 :  0.23772E+00 0.13249E+01
   Friction velocity        uet   :  0.14229E-01 0.78979E-01
   Friction velocity        uk    :  0.17752E-01 0.38828E-01
   Dimensionless distance   yplus :  0.43609E+03 0.95531E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60329E+01      55   0.13536E-02   0.19791E-01 
c  VelocityX    0.46304E+04      12   0.74685E-02   0.37716E-03 
c  VelocityY    0.46304E+04      12   0.74685E-02   0.25810E-04 
c  VelocityZ    0.46304E+04      12   0.74685E-02   0.39051E-04 
c  TurbEner     0.59730E+01      14   0.12390E-03   0.19503E-08 
c  Dissip       0.11920E+01      16   0.11351E-02   0.16433E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.16           54549           26779           27273
v  Velocity[x]            0.29271          2.1651         0.90806         0.90985
v  Velocity[y]           -0.38221         0.69313      0.00056183      0.00034028
v  Velocity[z]           -0.42119         0.51194      -0.0012385      -0.0013624
v  TurbEner             0.0010518        0.013545       0.0032863       0.0033457
v  Dissip               9.208e-05        0.022729      0.00044807       0.0003879
v  TurbVisc               0.17078          11.339          4.7164          5.2775
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              340:        0.95681E-01

===============================================================


 INSTANT    0.341000000E+03   TIME STEP NUMBER             341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999385E+04
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 :  0.23788E+00 0.12290E+01
   Friction velocity        uet   :  0.14238E-01 0.72281E-01
   Friction velocity        uk    :  0.17764E-01 0.38842E-01
   Dimensionless distance   yplus :  0.43555E+03 0.95504E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61304E+01      59   0.15134E-02   0.20109E-01 
c  VelocityX    0.46304E+04      12   0.66841E-02   0.40053E-03 
c  VelocityY    0.46304E+04      12   0.66841E-02   0.29350E-04 
c  VelocityZ    0.46304E+04      12   0.66841E-02   0.48892E-04 
c  TurbEner     0.59749E+01      14   0.11355E-03   0.22611E-08 
c  Dissip       0.12206E+01      17   0.13054E-02   0.27285E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.65           54523           26779           27273
v  Velocity[x]            0.29281          2.1914         0.90807         0.90985
v  Velocity[y]           -0.36612         0.70192      0.00055944      0.00033602
v  Velocity[z]           -0.42175         0.50651      -0.0012362      -0.0013531
v  TurbEner             0.0010529        0.014052       0.0032866       0.0033459
v  Dissip              9.2061e-05        0.023581      0.00044817      0.00038798
v  TurbVisc               0.17045          11.336          4.7166          5.2777
v  total_pressure           83081      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              341:        0.96112E-01

===============================================================


 INSTANT    0.342000000E+03   TIME STEP NUMBER             342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001063E+04
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 :  0.23770E+00 0.13247E+01
   Friction velocity        uet   :  0.14226E-01 0.78965E-01
   Friction velocity        uk    :  0.17773E-01 0.38836E-01
   Dimensionless distance   yplus :  0.43634E+03 0.95485E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62177E+01      62   0.14605E-02   0.20389E-01 
c  VelocityX    0.46304E+04      12   0.68886E-02   0.38446E-03 
c  VelocityY    0.46304E+04      12   0.68886E-02   0.26905E-04 
c  VelocityZ    0.46304E+04      12   0.68886E-02   0.40320E-04 
c  TurbEner     0.59758E+01      14   0.15667E-03   0.29729E-08 
c  Dissip       0.12497E+01      17   0.25493E-02   0.77257E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -167.5           54532           26778           27272
v  Velocity[x]            0.29256          2.0256         0.90804         0.90981
v  Velocity[y]           -0.38231         0.69165      0.00055396      0.00033487
v  Velocity[z]           -0.42285         0.51102      -0.0012485      -0.0013694
v  TurbEner             0.0010479        0.014972       0.0032869       0.0033462
v  Dissip              9.2062e-05        0.025551      0.00044842      0.00038818
v  TurbVisc               0.17082          11.313          4.7168          5.2779
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              342:        0.96954E-01

===============================================================


 INSTANT    0.343000000E+03   TIME STEP NUMBER             343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000451E+04
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 :  0.23771E+00 0.12164E+01
   Friction velocity        uet   :  0.14226E-01 0.72507E-01
   Friction velocity        uk    :  0.17730E-01 0.38784E-01
   Dimensionless distance   yplus :  0.43569E+03 0.95493E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61183E+01      55   0.12072E-02   0.20072E-01 
c  VelocityX    0.46304E+04      12   0.70185E-02   0.35813E-03 
c  VelocityY    0.46304E+04      12   0.70185E-02   0.42722E-04 
c  VelocityZ    0.46304E+04      12   0.70185E-02   0.37644E-04 
c  TurbEner     0.59757E+01      13   0.97641E-04   0.14384E-08 
c  Dissip       0.12474E+01      16   0.85402E-03   0.13149E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.65           54528           26778           27273
v  Velocity[x]             0.2928          2.0908         0.90807         0.90984
v  Velocity[y]           -0.36786         0.70018      0.00055774      0.00033601
v  Velocity[z]           -0.42073           0.504      -0.0012508      -0.0013684
v  TurbEner             0.0010491        0.014637       0.0032872       0.0033463
v  Dissip              9.2032e-05        0.025053      0.00044837      0.00038815
v  TurbVisc               0.17029          11.299          4.7171          5.2781
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              343:        0.95816E-01

===============================================================


 INSTANT    0.344000000E+03   TIME STEP NUMBER             344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999703E+04
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 :  0.23749E+00 0.13237E+01
   Friction velocity        uet   :  0.14211E-01 0.78904E-01
   Friction velocity        uk    :  0.17741E-01 0.38848E-01
   Dimensionless distance   yplus :  0.43524E+03 0.95410E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62814E+01      58   0.14072E-02   0.20591E-01 
c  VelocityX    0.46304E+04      12   0.69744E-02   0.39833E-03 
c  VelocityY    0.46304E+04      12   0.69744E-02   0.22433E-04 
c  VelocityZ    0.46304E+04      12   0.69744E-02   0.34387E-04 
c  TurbEner     0.59769E+01      13   0.65259E-04   0.93878E-09 
c  Dissip       0.12721E+01      16   0.80174E-03   0.14070E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.42           54510           26779           27273
v  Velocity[x]             0.2929          2.1482         0.90807         0.90985
v  Velocity[y]           -0.38262         0.69305      0.00055361      0.00033524
v  Velocity[z]           -0.42128         0.51157      -0.0012411      -0.0013608
v  TurbEner             0.0010478        0.014731       0.0032875       0.0033465
v  Dissip              9.2045e-05        0.025486      0.00044859       0.0003883
v  TurbVisc               0.17002          11.333          4.7173          5.2783
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              344:        0.96028E-01

===============================================================


 INSTANT    0.345000000E+03   TIME STEP NUMBER             345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998610E+04
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 :  0.23755E+00 0.12350E+01
   Friction velocity        uet   :  0.14214E-01 0.72531E-01
   Friction velocity        uk    :  0.17729E-01 0.38881E-01
   Dimensionless distance   yplus :  0.43549E+03 0.95384E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63286E+01      54   0.12605E-02   0.20755E-01 
c  VelocityX    0.46305E+04      12   0.73047E-02   0.35328E-03 
c  VelocityY    0.46305E+04      12   0.73047E-02   0.25943E-04 
c  VelocityZ    0.46305E+04      12   0.73047E-02   0.34493E-04 
c  TurbEner     0.59778E+01      14   0.87008E-04   0.18671E-08 
c  Dissip       0.13064E+01      17   0.13487E-02   0.39238E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.74           54518           26779           27273
v  Velocity[x]            0.29255          2.1731         0.90808         0.90986
v  Velocity[y]           -0.36669          0.7019      0.00054486      0.00032304
v  Velocity[z]           -0.42085         0.50588      -0.0012504      -0.0013673
v  TurbEner             0.0010432        0.014976       0.0032878       0.0033467
v  Dissip              9.2097e-05         0.02624      0.00044895      0.00038854
v  TurbVisc               0.17013          11.322          4.7176          5.2785
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              345:        0.95934E-01

===============================================================


 INSTANT    0.346000000E+03   TIME STEP NUMBER             346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001125E+04
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 :  0.23820E+00 0.13244E+01
   Friction velocity        uet   :  0.14252E-01 0.78946E-01
   Friction velocity        uk    :  0.17691E-01 0.38829E-01
   Dimensionless distance   yplus :  0.43497E+03 0.95330E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61824E+01      56   0.14381E-02   0.20274E-01 
c  VelocityX    0.46304E+04      12   0.70086E-02   0.42471E-03 
c  VelocityY    0.46304E+04      12   0.70086E-02   0.34348E-04 
c  VelocityZ    0.46304E+04      12   0.70086E-02   0.12157E-03 
c  TurbEner     0.59789E+01      14   0.12726E-03   0.19530E-08 
c  Dissip       0.13341E+01      17   0.22756E-02   0.68646E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.02           54522           26779           27273
v  Velocity[x]            0.29269          2.0148         0.90806         0.90984
v  Velocity[y]           -0.38244         0.69508      0.00055649      0.00033422
v  Velocity[z]           -0.42179         0.51089      -0.0012506       -0.001372
v  TurbEner              0.001043        0.015663       0.0032882       0.0033469
v  Dissip              9.2069e-05        0.028035      0.00044937      0.00038882
v  TurbVisc               0.16975          11.322          4.7177          5.2786
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              346:        0.95849E-01

===============================================================


 INSTANT    0.347000000E+03   TIME STEP NUMBER             347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999804E+04
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 :  0.23764E+00 0.12376E+01
   Friction velocity        uet   :  0.14217E-01 0.72513E-01
   Friction velocity        uk    :  0.17689E-01 0.38816E-01
   Dimensionless distance   yplus :  0.43402E+03 0.95305E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58637E+01      56   0.14674E-02   0.19232E-01 
c  VelocityX    0.46304E+04      13   0.62878E-02   0.37374E-03 
c  VelocityY    0.46304E+04      13   0.62878E-02   0.28728E-04 
c  VelocityZ    0.46304E+04      13   0.62878E-02   0.45299E-04 
c  TurbEner     0.59780E+01      14   0.11564E-03   0.18937E-08 
c  Dissip       0.13234E+01      16   0.12568E-02   0.26077E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.09           54514           26779           27273
v  Velocity[x]            0.29307          2.0933         0.90807         0.90985
v  Velocity[y]            -0.3676         0.70197      0.00056041      0.00033846
v  Velocity[z]           -0.42183         0.50439      -0.0012378      -0.0013535
v  TurbEner             0.0010443        0.015083       0.0032883        0.003347
v  Dissip              9.2078e-05        0.027202      0.00044942      0.00038885
v  TurbVisc               0.16933          11.352          4.7179          5.2787
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              347:        0.96509E-01

===============================================================


 INSTANT    0.348000000E+03   TIME STEP NUMBER             348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999374E+04
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 :  0.23748E+00 0.13259E+01
   Friction velocity        uet   :  0.14206E-01 0.79035E-01
   Friction velocity        uk    :  0.17700E-01 0.38831E-01
   Dimensionless distance   yplus :  0.43477E+03 0.95305E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56689E+01      52   0.12311E-02   0.18597E-01 
c  VelocityX    0.46305E+04      13   0.66837E-02   0.29234E-03 
c  VelocityY    0.46305E+04      13   0.66837E-02   0.22499E-04 
c  VelocityZ    0.46305E+04      13   0.66837E-02   0.30163E-04 
c  TurbEner     0.59779E+01      13   0.74562E-04   0.11020E-08 
c  Dissip       0.13423E+01      15   0.57268E-03   0.91402E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.62           54514           26779           27274
v  Velocity[x]            0.29252          2.1461         0.90806         0.90983
v  Velocity[y]           -0.38233         0.69567      0.00055803      0.00034001
v  Velocity[z]           -0.42174         0.51193      -0.0012447      -0.0013654
v  TurbEner             0.0010402        0.015007       0.0032885       0.0033471
v  Dissip              9.2113e-05        0.027412      0.00044969      0.00038901
v  TurbVisc               0.16985          11.335           4.718          5.2788
v  total_pressure           83077      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              348:        0.95918E-01

===============================================================


 INSTANT    0.349000000E+03   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998169E+04
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 :  0.23794E+00 0.12144E+01
   Friction velocity        uet   :  0.14232E-01 0.72333E-01
   Friction velocity        uk    :  0.17665E-01 0.38769E-01
   Dimensionless distance   yplus :  0.43415E+03 0.95234E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54078E+01      55   0.12754E-02   0.17735E-01 
c  VelocityX    0.46306E+04      12   0.76291E-02   0.30947E-03 
c  VelocityY    0.46306E+04      12   0.76291E-02   0.22344E-04 
c  VelocityZ    0.46306E+04      12   0.76291E-02   0.40658E-04 
c  TurbEner     0.59788E+01      13   0.69608E-04   0.91997E-09 
c  Dissip       0.13748E+01      16   0.11835E-02   0.30139E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.8           54520           26779           27273
v  Velocity[x]             0.2928          2.1692         0.90807         0.90984
v  Velocity[y]           -0.36612         0.70334      0.00055958      0.00033723
v  Velocity[z]           -0.42142         0.50653      -0.0012557      -0.0013742
v  TurbEner             0.0010434        0.015161       0.0032886       0.0033471
v  Dissip              9.2223e-05        0.028064      0.00045005      0.00038924
v  TurbVisc               0.16954          11.351           4.718          5.2788
v  total_pressure           83081      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              349:        0.95820E-01

===============================================================


 INSTANT    0.350000000E+03   TIME STEP NUMBER             350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001775E+04
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 :  0.23753E+00 0.13259E+01
   Friction velocity        uet   :  0.14206E-01 0.79038E-01
   Friction velocity        uk    :  0.17692E-01 0.38768E-01
   Dimensionless distance   yplus :  0.43391E+03 0.95229E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68720E+01      62   0.15868E-02   0.22526E-01 
c  VelocityX    0.46304E+04      12   0.73725E-02   0.43576E-03 
c  VelocityY    0.46304E+04      12   0.73725E-02   0.58915E-04 
c  VelocityZ    0.46304E+04      12   0.73725E-02   0.13542E-03 
c  TurbEner     0.59797E+01      13   0.11721E-03   0.14217E-08 
c  Dissip       0.14004E+01      16   0.21615E-02   0.58218E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.92           54520           26779           27273
v  Velocity[x]            0.29296           2.012         0.90805         0.90983
v  Velocity[y]           -0.38233         0.69277      0.00057617      0.00035436
v  Velocity[z]           -0.41923           0.511      -0.0012371      -0.0013582
v  TurbEner             0.0010449        0.015781        0.003289       0.0033474
v  Dissip              9.2236e-05        0.029799       0.0004505      0.00038955
v  TurbVisc               0.16959          11.332           4.718          5.2788
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              350:        0.96151E-01

===============================================================


 INSTANT    0.351000000E+03   TIME STEP NUMBER             351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999153E+04
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 :  0.23750E+00 0.12184E+01
   Friction velocity        uet   :  0.14204E-01 0.72594E-01
   Friction velocity        uk    :  0.17705E-01 0.38801E-01
   Dimensionless distance   yplus :  0.43456E+03 0.95212E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62167E+01      57   0.11952E-02   0.20387E-01 
c  VelocityX    0.46305E+04      12   0.62148E-02   0.42999E-03 
c  VelocityY    0.46305E+04      12   0.62148E-02   0.33666E-04 
c  VelocityZ    0.46305E+04      12   0.62148E-02   0.57752E-04 
c  TurbEner     0.59783E+01      13   0.12542E-03   0.20453E-08 
c  Dissip       0.13828E+01      16   0.15012E-02   0.36401E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.49           54512           26779           27273
v  Velocity[x]            0.29257          2.0883         0.90808         0.90985
v  Velocity[y]           -0.36787          0.7001      0.00055639      0.00033165
v  Velocity[z]           -0.42063         0.50397      -0.0012536      -0.0013712
v  TurbEner             0.0010444        0.015179       0.0032889       0.0033474
v  Dissip              9.2209e-05        0.028801       0.0004505      0.00038955
v  TurbVisc               0.17011          11.329          4.7181          5.2789
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              351:        0.95651E-01

===============================================================


 INSTANT    0.352000000E+03   TIME STEP NUMBER             352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001726E+04
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 :  0.23792E+00 0.13240E+01
   Friction velocity        uet   :  0.14229E-01 0.78915E-01
   Friction velocity        uk    :  0.17701E-01 0.38813E-01
   Dimensionless distance   yplus :  0.43480E+03 0.95164E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55376E+01      56   0.13267E-02   0.18157E-01 
c  VelocityX    0.46306E+04      12   0.70614E-02   0.36404E-03 
c  VelocityY    0.46306E+04      12   0.70614E-02   0.23862E-04 
c  VelocityZ    0.46306E+04      12   0.70614E-02   0.29304E-04 
c  TurbEner     0.59785E+01      12   0.61075E-04   0.62902E-09 
c  Dissip       0.13969E+01      14   0.39252E-03   0.42478E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.34           54521           26779           27273
v  Velocity[x]            0.29268          2.1458         0.90807         0.90984
v  Velocity[y]           -0.38297         0.69484      0.00055148      0.00033224
v  Velocity[z]           -0.42219         0.51129      -0.0012476      -0.0013672
v  TurbEner             0.0010483        0.015028       0.0032889       0.0033473
v  Dissip              9.2179e-05        0.028774      0.00045067      0.00038966
v  TurbVisc               0.17029          11.362          4.7181          5.2789
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              352:        0.95472E-01

===============================================================


 INSTANT    0.353000000E+03   TIME STEP NUMBER             353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000410E+04
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 :  0.23758E+00 0.12126E+01
   Friction velocity        uet   :  0.14209E-01 0.72280E-01
   Friction velocity        uk    :  0.17733E-01 0.38800E-01
   Dimensionless distance   yplus :  0.43469E+03 0.95225E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59294E+01      56   0.14451E-02   0.19451E-01 
c  VelocityX    0.46305E+04      13   0.74342E-02   0.31005E-03 
c  VelocityY    0.46305E+04      13   0.74342E-02   0.24402E-04 
c  VelocityZ    0.46305E+04      13   0.74342E-02   0.44332E-04 
c  TurbEner     0.59796E+01      13   0.68248E-04   0.97363E-09 
c  Dissip       0.14237E+01      16   0.98025E-03   0.21193E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.79           54509           26778           27273
v  Velocity[x]            0.29322          2.1694         0.90806         0.90984
v  Velocity[y]           -0.36812         0.70421      0.00055514      0.00033279
v  Velocity[z]           -0.42144         0.50695      -0.0012466      -0.0013651
v  TurbEner             0.0010528        0.015142        0.003289       0.0033475
v  Dissip              9.2137e-05        0.029275      0.00045099      0.00038987
v  TurbVisc               0.17039          11.339           4.718          5.2789
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              353:        0.96176E-01

===============================================================


 INSTANT    0.354000000E+03   TIME STEP NUMBER             354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000525E+04
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 :  0.23786E+00 0.13249E+01
   Friction velocity        uet   :  0.14226E-01 0.78973E-01
   Friction velocity        uk    :  0.17772E-01 0.38820E-01
   Dimensionless distance   yplus :  0.43616E+03 0.95282E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67346E+01      56   0.14470E-02   0.22091E-01 
c  VelocityX    0.46304E+04      13   0.66014E-02   0.40610E-03 
c  VelocityY    0.46304E+04      13   0.66014E-02   0.56973E-04 
c  VelocityZ    0.46304E+04      13   0.66014E-02   0.13993E-03 
c  TurbEner     0.59793E+01      13   0.12029E-03   0.14114E-08 
c  Dissip       0.14453E+01      16   0.21052E-02   0.51626E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.37           54517           26779           27273
v  Velocity[x]            0.29281          2.0113         0.90805         0.90982
v  Velocity[y]           -0.38274         0.69185      0.00055716      0.00033518
v  Velocity[z]           -0.42158         0.51371      -0.0012402        -0.00136
v  TurbEner              0.001051         0.01575        0.003289       0.0033475
v  Dissip              9.2124e-05        0.030969      0.00045131       0.0003901
v  TurbVisc               0.17131          11.321           4.718          5.2789
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              354:        0.95927E-01

===============================================================


 INSTANT    0.355000000E+03   TIME STEP NUMBER             355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999610E+04
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 :  0.23799E+00 0.12178E+01
   Friction velocity        uet   :  0.14235E-01 0.72583E-01
   Friction velocity        uk    :  0.17757E-01 0.38727E-01
   Dimensionless distance   yplus :  0.43614E+03 0.95265E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55939E+01      56   0.12860E-02   0.18349E-01 
c  VelocityX    0.46304E+04      12   0.66445E-02   0.37275E-03 
c  VelocityY    0.46304E+04      12   0.66445E-02   0.29929E-04 
c  VelocityZ    0.46304E+04      12   0.66445E-02   0.54827E-04 
c  TurbEner     0.59781E+01      13   0.13431E-03   0.18814E-08 
c  Dissip       0.14233E+01      16   0.16732E-02   0.42154E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.41           54515           26778           27273
v  Velocity[x]            0.29262          2.0877         0.90805         0.90983
v  Velocity[y]           -0.36654         0.70084      0.00055247      0.00033083
v  Velocity[z]           -0.42121         0.50794      -0.0012558      -0.0013764
v  TurbEner             0.0010558        0.015136       0.0032887       0.0033473
v  Dissip              9.2086e-05        0.029841       0.0004512      0.00039001
v  TurbVisc               0.17127          11.362          4.7179          5.2787
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              355:        0.95780E-01

===============================================================


 INSTANT    0.356000000E+03   TIME STEP NUMBER             356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001838E+04
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 :  0.23777E+00 0.13239E+01
   Friction velocity        uet   :  0.14222E-01 0.78914E-01
   Friction velocity        uk    :  0.17797E-01 0.38749E-01
   Dimensionless distance   yplus :  0.43632E+03 0.95285E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58281E+01      58   0.14122E-02   0.19112E-01 
c  VelocityX    0.46304E+04      12   0.66178E-02   0.35961E-03 
c  VelocityY    0.46304E+04      12   0.66178E-02   0.23666E-04 
c  VelocityZ    0.46304E+04      12   0.66178E-02   0.33139E-04 
c  TurbEner     0.59783E+01      13   0.69249E-04   0.82030E-09 
c  Dissip       0.14350E+01      14   0.38329E-03   0.34962E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.41           54506           26778           27273
v  Velocity[x]            0.29277          2.1461         0.90806         0.90984
v  Velocity[y]           -0.38277         0.69464      0.00055457      0.00033623
v  Velocity[z]           -0.42029         0.51204      -0.0012331       -0.001352
v  TurbEner              0.001058         0.01497       0.0032887       0.0033473
v  Dissip               9.207e-05        0.029718      0.00045135      0.00039012
v  TurbVisc               0.17148          11.349          4.7177          5.2786
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              356:        0.95313E-01

===============================================================


 INSTANT    0.357000000E+03   TIME STEP NUMBER             357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999939E+04
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 :  0.23744E+00 0.12173E+01
   Friction velocity        uet   :  0.14204E-01 0.72566E-01
   Friction velocity        uk    :  0.17815E-01 0.38771E-01
   Dimensionless distance   yplus :  0.43724E+03 0.95280E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57840E+01      56   0.12287E-02   0.18970E-01 
c  VelocityX    0.46304E+04      13   0.71653E-02   0.28879E-03 
c  VelocityY    0.46304E+04      13   0.71653E-02   0.24785E-04 
c  VelocityZ    0.46304E+04      13   0.71653E-02   0.44643E-04 
c  TurbEner     0.59784E+01      13   0.69786E-04   0.97886E-09 
c  Dissip       0.14577E+01      15   0.82193E-03   0.15444E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.65           54508           26777           27272
v  Velocity[x]            0.29284          2.1719         0.90805         0.90983
v  Velocity[y]           -0.36835         0.70354      0.00054675      0.00032685
v  Velocity[z]           -0.42193         0.50475      -0.0012515      -0.0013688
v  TurbEner             0.0010566        0.015056       0.0032886       0.0033472
v  Dissip              9.2048e-05        0.030089      0.00045154      0.00039024
v  TurbVisc               0.17203          11.349          4.7176          5.2786
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              357:        0.96381E-01

===============================================================


 INSTANT    0.358000000E+03   TIME STEP NUMBER             358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001896E+04
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 :  0.23769E+00 0.13236E+01
   Friction velocity        uet   :  0.14220E-01 0.78899E-01
   Friction velocity        uk    :  0.17804E-01 0.38799E-01
   Dimensionless distance   yplus :  0.43737E+03 0.95235E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64072E+01      54   0.15221E-02   0.21013E-01 
c  VelocityX    0.46303E+04      12   0.78366E-02   0.40997E-03 
c  VelocityY    0.46303E+04      12   0.78366E-02   0.57282E-04 
c  VelocityZ    0.46303E+04      12   0.78366E-02   0.13279E-03 
c  TurbEner     0.59791E+01      13   0.11362E-03   0.10786E-08 
c  Dissip       0.14756E+01      16   0.19873E-02   0.43966E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.35           54520           26778           27272
v  Velocity[x]             0.2927          2.0136         0.90805         0.90983
v  Velocity[y]           -0.38265         0.69601      0.00056069      0.00033953
v  Velocity[z]           -0.42124         0.51223      -0.0012422      -0.0013652
v  TurbEner             0.0010585        0.015643       0.0032886       0.0033472
v  Dissip              9.2047e-05        0.031678      0.00045179      0.00039042
v  TurbVisc               0.17201          11.382          4.7175          5.2785
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              358:        0.95205E-01

===============================================================


 INSTANT    0.359000000E+03   TIME STEP NUMBER             359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998127E+04
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 :  0.23793E+00 0.12173E+01
   Friction velocity        uet   :  0.14235E-01 0.72567E-01
   Friction velocity        uk    :  0.17820E-01 0.38809E-01
   Dimensionless distance   yplus :  0.43695E+03 0.95259E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65558E+01      54   0.14716E-02   0.21493E-01 
c  VelocityX    0.46302E+04      12   0.69890E-02   0.41695E-03 
c  VelocityY    0.46302E+04      12   0.69890E-02   0.31180E-04 
c  VelocityZ    0.46302E+04      12   0.69890E-02   0.59254E-04 
c  TurbEner     0.59778E+01      13   0.13069E-03   0.19199E-08 
c  Dissip       0.14492E+01      16   0.18476E-02   0.49329E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.39           54510           26778           27272
v  Velocity[x]            0.29304          2.0895         0.90806         0.90984
v  Velocity[y]           -0.36665         0.70135      0.00055834      0.00033385
v  Velocity[z]           -0.42122         0.50637      -0.0012394      -0.0013581
v  TurbEner             0.0010609        0.015041       0.0032884        0.003347
v  Dissip              9.2081e-05        0.030428      0.00045161      0.00039029
v  TurbVisc                0.1718           11.36          4.7175          5.2784
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              359:        0.95849E-01

===============================================================


 INSTANT    0.360000000E+03   TIME STEP NUMBER             360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001384E+04
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 :  0.23759E+00 0.13260E+01
   Friction velocity        uet   :  0.14216E-01 0.79035E-01
   Friction velocity        uk    :  0.17841E-01 0.38710E-01
   Dimensionless distance   yplus :  0.43804E+03 0.95215E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61445E+01      62   0.11832E-02   0.20142E-01 
c  VelocityX    0.46304E+04      12   0.71753E-02   0.37616E-03 
c  VelocityY    0.46304E+04      12   0.71753E-02   0.29326E-04 
c  VelocityZ    0.46304E+04      12   0.71753E-02   0.33767E-04 
c  TurbEner     0.59777E+01      12   0.66798E-04   0.81466E-09 
c  Dissip       0.14568E+01      13   0.46680E-03   0.35933E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.54           54514           26778           27272
v  Velocity[x]            0.29258          2.1487         0.90806         0.90984
v  Velocity[y]           -0.38248         0.69291      0.00054961      0.00032952
v  Velocity[z]           -0.42222         0.51125      -0.0012446       -0.001367
v  TurbEner             0.0010563         0.01486       0.0032882       0.0033469
v  Dissip              9.2082e-05        0.030165      0.00045168      0.00039035
v  TurbVisc               0.17236          11.361          4.7173          5.2784
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              360:        0.96722E-01

===============================================================


 INSTANT    0.361000000E+03   TIME STEP NUMBER             361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999621E+04
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 :  0.23779E+00 0.12160E+01
   Friction velocity        uet   :  0.14229E-01 0.72479E-01
   Friction velocity        uk    :  0.17801E-01 0.38655E-01
   Dimensionless distance   yplus :  0.43750E+03 0.95217E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58946E+01      53   0.12712E-02   0.19326E-01 
c  VelocityX    0.46303E+04      12   0.73050E-02   0.32330E-03 
c  VelocityY    0.46303E+04      12   0.73050E-02   0.28723E-04 
c  VelocityZ    0.46303E+04      12   0.73050E-02   0.32718E-04 
c  TurbEner     0.59786E+01      13   0.64992E-04   0.91174E-09 
c  Dissip       0.14774E+01      15   0.81226E-03   0.14384E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.99           54514           26777           27272
v  Velocity[x]            0.29271          2.1707         0.90806         0.90984
v  Velocity[y]           -0.36775         0.70103      0.00055266      0.00032792
v  Velocity[z]           -0.42048         0.50446      -0.0012495      -0.0013691
v  TurbEner             0.0010578         0.01497       0.0032883        0.003347
v  Dissip              9.2077e-05         0.03055      0.00045182      0.00039045
v  TurbVisc               0.17188           11.33          4.7172          5.2782
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              361:        0.95719E-01

===============================================================


 INSTANT    0.362000000E+03   TIME STEP NUMBER             362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001055E+04
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 :  0.23744E+00 0.13233E+01
   Friction velocity        uet   :  0.14209E-01 0.78877E-01
   Friction velocity        uk    :  0.17814E-01 0.38672E-01
   Dimensionless distance   yplus :  0.43705E+03 0.95198E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66298E+01      63   0.15316E-02   0.21743E-01 
c  VelocityX    0.46302E+04      12   0.73674E-02   0.43449E-03 
c  VelocityY    0.46302E+04      12   0.73674E-02   0.30327E-04 
c  VelocityZ    0.46302E+04      12   0.73674E-02   0.73203E-04 
c  TurbEner     0.59794E+01      13   0.12200E-03   0.15824E-08 
c  Dissip       0.14962E+01      16   0.20113E-02   0.44116E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.16           54511           26778           27272
v  Velocity[x]            0.29277           2.014         0.90805         0.90983
v  Velocity[y]           -0.38227         0.69411      0.00056063      0.00033957
v  Velocity[z]           -0.42085         0.51196      -0.0012432      -0.0013641
v  TurbEner             0.0010563        0.015545       0.0032883       0.0033471
v  Dissip              9.2095e-05         0.03215      0.00045206      0.00039063
v  TurbVisc               0.17158          11.324          4.7172          5.2782
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              362:        0.97861E-01

===============================================================


 INSTANT    0.363000000E+03   TIME STEP NUMBER             363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998712E+04
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 :  0.23756E+00 0.12159E+01
   Friction velocity        uet   :  0.14217E-01 0.72486E-01
   Friction velocity        uk    :  0.17801E-01 0.38718E-01
   Dimensionless distance   yplus :  0.43721E+03 0.95162E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61248E+01      56   0.12157E-02   0.20092E-01 
c  VelocityX    0.46302E+04      12   0.68204E-02   0.36684E-03 
c  VelocityY    0.46302E+04      12   0.68204E-02   0.28407E-04 
c  VelocityZ    0.46302E+04      12   0.68204E-02   0.98269E-04 
c  TurbEner     0.59772E+01      14   0.15030E-03   0.23728E-08 
c  Dissip       0.14608E+01      17   0.23776E-02   0.73670E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.44           54519           26778           27272
v  Velocity[x]            0.29265          2.0971         0.90805         0.90983
v  Velocity[y]           -0.36606          0.7003      0.00056064      0.00033721
v  Velocity[z]           -0.42067         0.50665      -0.0012471      -0.0013677
v  TurbEner             0.0010515        0.014834        0.003288       0.0033468
v  Dissip              9.2079e-05        0.030505       0.0004518      0.00039045
v  TurbVisc               0.17157          11.364           4.717          5.2781
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              363:        0.95847E-01

===============================================================


 INSTANT    0.364000000E+03   TIME STEP NUMBER             364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001249E+04
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 :  0.23821E+00 0.13253E+01
   Friction velocity        uet   :  0.14256E-01 0.79003E-01
   Friction velocity        uk    :  0.17761E-01 0.38751E-01
   Dimensionless distance   yplus :  0.43667E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62020E+01      56   0.13449E-02   0.20332E-01 
c  VelocityX    0.46302E+04      12   0.74935E-02   0.37369E-03 
c  VelocityY    0.46302E+04      12   0.74935E-02   0.22321E-04 
c  VelocityZ    0.46302E+04      12   0.74935E-02   0.37469E-04 
c  TurbEner     0.59773E+01      12   0.59222E-04   0.63570E-09 
c  Dissip       0.14648E+01      13   0.25975E-03   0.16796E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.05           54518           26778           27272
v  Velocity[x]            0.29267          2.1467         0.90805         0.90984
v  Velocity[y]           -0.38238         0.69367      0.00055447      0.00033238
v  Velocity[z]           -0.42178         0.51111      -0.0012471      -0.0013714
v  TurbEner             0.0010498        0.014799       0.0032878       0.0033466
v  Dissip                9.21e-05        0.030471      0.00045176      0.00039043
v  TurbVisc               0.17106          11.348          4.7168          5.2779
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              364:        0.94368E-01

===============================================================


 INSTANT    0.365000000E+03   TIME STEP NUMBER             365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997597E+04
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 :  0.23771E+00 0.12143E+01
   Friction velocity        uet   :  0.14227E-01 0.72307E-01
   Friction velocity        uk    :  0.17747E-01 0.38717E-01
   Dimensionless distance   yplus :  0.43558E+03 0.95266E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59564E+01      53   0.13586E-02   0.19537E-01 
c  VelocityX    0.46301E+04      13   0.68586E-02   0.36166E-03 
c  VelocityY    0.46301E+04      13   0.68586E-02   0.26667E-04 
c  VelocityZ    0.46301E+04      13   0.68586E-02   0.48783E-04 
c  TurbEner     0.59780E+01      13   0.77621E-04   0.12048E-08 
c  Dissip       0.14901E+01      15   0.88024E-03   0.17857E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.69           54509           26778           27272
v  Velocity[x]            0.29273          2.1804         0.90804         0.90983
v  Velocity[y]           -0.36814         0.70215      0.00056056      0.00033671
v  Velocity[z]           -0.42169           0.504      -0.0012496       -0.001367
v  TurbEner             0.0010488        0.014888       0.0032877       0.0033466
v  Dissip              9.2101e-05        0.030813       0.0004519      0.00039053
v  TurbVisc               0.17037          11.353          4.7166          5.2777
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              365:        0.95568E-01

===============================================================


 INSTANT    0.366000000E+03   TIME STEP NUMBER             366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999000E+04
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 :  0.23745E+00 0.13249E+01
   Friction velocity        uet   :  0.14212E-01 0.78977E-01
   Friction velocity        uk    :  0.17738E-01 0.38712E-01
   Dimensionless distance   yplus :  0.43600E+03 0.95243E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69340E+01      63   0.14797E-02   0.22725E-01 
c  VelocityX    0.46301E+04      12   0.75568E-02   0.40196E-03 
c  VelocityY    0.46301E+04      12   0.75568E-02   0.36488E-04 
c  VelocityZ    0.46301E+04      12   0.75568E-02   0.48256E-04 
c  TurbEner     0.59782E+01      13   0.11809E-03   0.13682E-08 
c  Dissip       0.15081E+01      16   0.19792E-02   0.43928E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.16           54515           26778           27272
v  Velocity[x]            0.29283          2.0241         0.90804         0.90982
v  Velocity[y]           -0.38256         0.69181      0.00055827      0.00033608
v  Velocity[z]           -0.42173         0.51166      -0.0012555      -0.0013811
v  TurbEner              0.001041        0.015435       0.0032876       0.0033466
v  Dissip               9.209e-05        0.032364       0.0004521      0.00039068
v  TurbVisc               0.17048          11.326          4.7164          5.2775
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              366:        0.97765E-01

===============================================================


 INSTANT    0.367000000E+03   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999944E+04
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 :  0.23787E+00 0.12169E+01
   Friction velocity        uet   :  0.14237E-01 0.72539E-01
   Friction velocity        uk    :  0.17672E-01 0.38637E-01
   Dimensionless distance   yplus :  0.43482E+03 0.95278E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64911E+01      57   0.14110E-02   0.21277E-01 
c  VelocityX    0.46301E+04      12   0.73154E-02   0.40196E-03 
c  VelocityY    0.46301E+04      12   0.73154E-02   0.42218E-04 
c  VelocityZ    0.46301E+04      12   0.73154E-02   0.42597E-04 
c  TurbEner     0.59768E+01      13   0.13941E-03   0.19710E-08 
c  Dissip       0.14734E+01      16   0.21445E-02   0.64020E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.39           54508           26777           27271
v  Velocity[x]            0.29281          2.0906         0.90807         0.90984
v  Velocity[y]           -0.36662         0.69916        0.000549      0.00032542
v  Velocity[z]           -0.42247         0.50592      -0.0012672      -0.0013863
v  TurbEner             0.0010399        0.014818       0.0032874       0.0033464
v  Dissip              9.2076e-05        0.030941      0.00045183      0.00039049
v  TurbVisc               0.16959          11.317          4.7163          5.2773
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              367:        0.96074E-01

===============================================================


 INSTANT    0.368000000E+03   TIME STEP NUMBER             368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002291E+04
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 :  0.23759E+00 0.13238E+01
   Friction velocity        uet   :  0.14221E-01 0.78908E-01
   Friction velocity        uk    :  0.17663E-01 0.38698E-01
   Dimensionless distance   yplus :  0.43383E+03 0.95267E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68170E+01      57   0.15097E-02   0.22350E-01 
c  VelocityX    0.46301E+04      12   0.71485E-02   0.44631E-03 
c  VelocityY    0.46301E+04      12   0.71485E-02   0.33445E-04 
c  VelocityZ    0.46301E+04      12   0.71485E-02   0.34480E-04 
c  TurbEner     0.59772E+01      12   0.67180E-04   0.84261E-09 
c  Dissip       0.14809E+01      13   0.40836E-03   0.26520E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.29           54512           26777           27272
v  Velocity[x]            0.29261          2.1502         0.90808         0.90985
v  Velocity[y]           -0.38249         0.69246      0.00055242      0.00033318
v  Velocity[z]           -0.41913         0.51097      -0.0012454      -0.0013659
v  TurbEner             0.0010368        0.014704       0.0032874       0.0033464
v  Dissip              9.2063e-05          0.0307       0.0004518      0.00039048
v  TurbVisc               0.16903          11.344          4.7161          5.2771
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              368:        0.95336E-01

===============================================================


 INSTANT    0.369000000E+03   TIME STEP NUMBER             369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999814E+04
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 :  0.23766E+00 0.12160E+01
   Friction velocity        uet   :  0.14225E-01 0.72493E-01
   Friction velocity        uk    :  0.17637E-01 0.38778E-01
   Dimensionless distance   yplus :  0.43368E+03 0.95288E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60605E+01      54   0.11810E-02   0.19870E-01 
c  VelocityX    0.46301E+04      12   0.73374E-02   0.34560E-03 
c  VelocityY    0.46301E+04      12   0.73374E-02   0.28345E-04 
c  VelocityZ    0.46301E+04      12   0.73374E-02   0.81965E-04 
c  TurbEner     0.59775E+01      13   0.86945E-04   0.12612E-08 
c  Dissip       0.15007E+01      15   0.76906E-03   0.13910E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.56           54519           26777           27271
v  Velocity[x]            0.29256          2.1782         0.90807         0.90984
v  Velocity[y]           -0.36781         0.70151       0.0005485      0.00032509
v  Velocity[z]           -0.42156         0.50426      -0.0012569      -0.0013751
v  TurbEner              0.001031        0.014843       0.0032873       0.0033463
v  Dissip              9.2038e-05        0.030984       0.0004519      0.00039054
v  TurbVisc                0.1689          11.391           4.716          5.2769
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              369:        0.95470E-01

===============================================================


 INSTANT    0.370000000E+03   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000125E+04
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 :  0.23768E+00 0.13234E+01
   Friction velocity        uet   :  0.14226E-01 0.78886E-01
   Friction velocity        uk    :  0.17587E-01 0.38796E-01
   Dimensionless distance   yplus :  0.43284E+03 0.95296E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64938E+01      57   0.14139E-02   0.21286E-01 
c  VelocityX    0.46300E+04      12   0.64609E-02   0.37796E-03 
c  VelocityY    0.46300E+04      12   0.64609E-02   0.21553E-04 
c  VelocityZ    0.46300E+04      12   0.64609E-02   0.60040E-04 
c  TurbEner     0.59782E+01      13   0.12864E-03   0.14678E-08 
c  Dissip       0.15148E+01      16   0.21664E-02   0.49758E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.68           54520           26777           27271
v  Velocity[x]            0.29302          2.0169         0.90805         0.90982
v  Velocity[y]            -0.3823         0.69439       0.0005539      0.00033011
v  Velocity[z]           -0.42282         0.51183      -0.0012625      -0.0013828
v  TurbEner             0.0010293        0.015466       0.0032873       0.0033463
v  Dissip              9.2057e-05        0.032689      0.00045212      0.00039071
v  TurbVisc               0.16823          11.378          4.7157          5.2767
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              370:        0.96088E-01

===============================================================


 INSTANT    0.371000000E+03   TIME STEP NUMBER             371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001117E+04
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 :  0.23770E+00 0.12163E+01
   Friction velocity        uet   :  0.14228E-01 0.72510E-01
   Friction velocity        uk    :  0.17573E-01 0.38778E-01
   Dimensionless distance   yplus :  0.43157E+03 0.95255E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56489E+01      53   0.11482E-02   0.18525E-01 
c  VelocityX    0.46299E+04      12   0.61549E-02   0.30451E-03 
c  VelocityY    0.46299E+04      12   0.61549E-02   0.24722E-04 
c  VelocityZ    0.46299E+04      12   0.61549E-02   0.45504E-04 
c  TurbEner     0.59769E+01      14   0.15624E-03   0.24855E-08 
c  Dissip       0.14782E+01      16   0.23603E-02   0.72794E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.14           54535           26776           27271
v  Velocity[x]            0.29289          2.0926         0.90806         0.90984
v  Velocity[y]           -0.36612         0.70137      0.00054374      0.00032133
v  Velocity[z]           -0.42075         0.50647      -0.0012647      -0.0013807
v  TurbEner             0.0010291        0.014756       0.0032872       0.0033462
v  Dissip              9.2007e-05        0.031084      0.00045186      0.00039053
v  TurbVisc                0.1676          11.328          4.7155          5.2765
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              371:        0.95324E-01

===============================================================


 INSTANT    0.372000000E+03   TIME STEP NUMBER             372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001004E+04
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 :  0.23792E+00 0.13259E+01
   Friction velocity        uet   :  0.14241E-01 0.79034E-01
   Friction velocity        uk    :  0.17571E-01 0.38699E-01
   Dimensionless distance   yplus :  0.43198E+03 0.95287E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57455E+01      52   0.12751E-02   0.18833E-01 
c  VelocityX    0.46300E+04      12   0.72035E-02   0.28764E-03 
c  VelocityY    0.46300E+04      12   0.72035E-02   0.30067E-04 
c  VelocityZ    0.46300E+04      12   0.72035E-02   0.30965E-04 
c  TurbEner     0.59772E+01      13   0.68206E-04   0.82930E-09 
c  Dissip       0.14837E+01      13   0.44880E-03   0.27756E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.47           54545           26776           27271
v  Velocity[x]            0.29265          2.1484         0.90806         0.90984
v  Velocity[y]           -0.38247         0.69454      0.00054226      0.00032261
v  Velocity[z]           -0.42244         0.51089      -0.0012561      -0.0013767
v  TurbEner             0.0010228        0.014623       0.0032871       0.0033462
v  Dissip              9.2005e-05        0.030802      0.00045183      0.00039052
v  TurbVisc               0.16779          11.317          4.7154          5.2763
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              372:        0.94837E-01

===============================================================


 INSTANT    0.373000000E+03   TIME STEP NUMBER             373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999386E+04
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 :  0.23769E+00 0.12143E+01
   Friction velocity        uet   :  0.14227E-01 0.72333E-01
   Friction velocity        uk    :  0.17517E-01 0.38682E-01
   Dimensionless distance   yplus :  0.43097E+03 0.95285E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67350E+01      60   0.15579E-02   0.22081E-01 
c  VelocityX    0.46300E+04      13   0.75118E-02   0.47703E-03 
c  VelocityY    0.46300E+04      13   0.75118E-02   0.36897E-04 
c  VelocityZ    0.46300E+04      13   0.75118E-02   0.35850E-04 
c  TurbEner     0.59775E+01      13   0.10148E-03   0.12442E-08 
c  Dissip       0.14890E+01      16   0.15269E-02   0.28691E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.31           54538           26776           27271
v  Velocity[x]            0.29272          1.9952         0.90808         0.90985
v  Velocity[y]           -0.36813         0.70316      0.00054555      0.00032383
v  Velocity[z]           -0.42095         0.50387      -0.0012636      -0.0013812
v  TurbEner             0.0010236        0.015059        0.003287       0.0033462
v  Dissip              9.2033e-05        0.031908       0.0004519      0.00039059
v  TurbVisc               0.16706          11.347          4.7151          5.2761
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              373:        0.96499E-01

===============================================================


 INSTANT    0.374000000E+03   TIME STEP NUMBER             374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999950E+04
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 :  0.23778E+00 0.13254E+01
   Friction velocity        uet   :  0.14233E-01 0.79004E-01
   Friction velocity        uk    :  0.17524E-01 0.38748E-01
   Dimensionless distance   yplus :  0.43024E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62452E+01      64   0.15642E-02   0.20476E-01 
c  VelocityX    0.46299E+04      12   0.66160E-02   0.39486E-03 
c  VelocityY    0.46299E+04      12   0.66160E-02   0.25900E-04 
c  VelocityZ    0.46299E+04      12   0.66160E-02   0.57426E-04 
c  TurbEner     0.59765E+01      14   0.13513E-03   0.24399E-08 
c  Dissip       0.14503E+01      17   0.24029E-02   0.79396E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.95           54515           26778           27272
v  Velocity[x]            0.29285          2.0767         0.90806         0.90983
v  Velocity[y]           -0.38296         0.69266      0.00054363      0.00032456
v  Velocity[z]           -0.41996         0.51127      -0.0012452      -0.0013646
v  TurbEner             0.0010228        0.014486       0.0032868       0.0033462
v  Dissip              9.2056e-05        0.030387       0.0004516       0.0003904
v  TurbVisc               0.16668          11.331          4.7149          5.2758
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              374:        0.97948E-01

===============================================================


 INSTANT    0.375000000E+03   TIME STEP NUMBER             375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997998E+04
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 :  0.23719E+00 0.12175E+01
   Friction velocity        uet   :  0.14198E-01 0.72573E-01
   Friction velocity        uk    :  0.17517E-01 0.38770E-01
   Dimensionless distance   yplus :  0.43045E+03 0.95243E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64522E+01      55   0.13640E-02   0.21161E-01 
c  VelocityX    0.46299E+04      13   0.68035E-02   0.31894E-03 
c  VelocityY    0.46299E+04      13   0.68035E-02   0.40314E-04 
c  VelocityZ    0.46299E+04      13   0.68035E-02   0.95401E-04 
c  TurbEner     0.59761E+01      13   0.73190E-04   0.95894E-09 
c  Dissip       0.14493E+01      14   0.86637E-03   0.77399E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.95           54522           26778           27272
v  Velocity[x]            0.29267          2.1359         0.90803          0.9098
v  Velocity[y]           -0.36797         0.70085      0.00055461      0.00033279
v  Velocity[z]           -0.42168           0.507      -0.0012541      -0.0013735
v  TurbEner              0.001019        0.014361       0.0032866       0.0033461
v  Dissip              9.2086e-05        0.029786      0.00045147      0.00039032
v  TurbVisc               0.16674           11.33          4.7147          5.2757
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              375:        0.96110E-01

===============================================================


 INSTANT    0.376000000E+03   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998013E+04
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 :  0.23763E+00 0.13239E+01
   Friction velocity        uet   :  0.14224E-01 0.78914E-01
   Friction velocity        uk    :  0.17484E-01 0.38753E-01
   Dimensionless distance   yplus :  0.43000E+03 0.95252E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64851E+01      56   0.13404E-02   0.21264E-01 
c  VelocityX    0.46299E+04      13   0.68233E-02   0.38665E-03 
c  VelocityY    0.46299E+04      13   0.68233E-02   0.47743E-04 
c  VelocityZ    0.46299E+04      13   0.68233E-02   0.45954E-04 
c  TurbEner     0.59766E+01      13   0.78149E-04   0.10466E-08 
c  Dissip       0.14595E+01      15   0.61484E-03   0.91393E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.05           54534           26778           27273
v  Velocity[x]            0.29274          2.1678         0.90805         0.90983
v  Velocity[y]           -0.38279         0.69615      0.00055156      0.00032945
v  Velocity[z]           -0.42106         0.51386      -0.0012525      -0.0013733
v  TurbEner             0.0010192        0.014545       0.0032865        0.003346
v  Dissip               9.208e-05         0.02994      0.00045153      0.00039037
v  TurbVisc               0.16634          11.358          4.7145          5.2755
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              376:        0.96476E-01

===============================================================


 INSTANT    0.377000000E+03   TIME STEP NUMBER             377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997797E+04
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 :  0.23796E+00 0.12136E+01
   Friction velocity        uet   :  0.14244E-01 0.72349E-01
   Friction velocity        uk    :  0.17486E-01 0.38735E-01
   Dimensionless distance   yplus :  0.42915E+03 0.95227E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56128E+01      57   0.12821E-02   0.18384E-01 
c  VelocityX    0.46300E+04      12   0.71048E-02   0.32600E-03 
c  VelocityY    0.46300E+04      12   0.71048E-02   0.33547E-04 
c  VelocityZ    0.46300E+04      12   0.71048E-02   0.41589E-04 
c  TurbEner     0.59775E+01      13   0.98098E-04   0.10636E-08 
c  Dissip       0.14799E+01      15   0.78184E-03   0.11749E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.61           54540           26777           27271
v  Velocity[x]            0.29294          2.2011         0.90805         0.90984
v  Velocity[y]           -0.36653         0.70416      0.00055146      0.00032737
v  Velocity[z]           -0.42169          0.5079      -0.0012499      -0.0013704
v  TurbEner             0.0010205         0.01476       0.0032863       0.0033458
v  Dissip              9.2129e-05        0.030351       0.0004516      0.00039042
v  TurbVisc               0.16586          11.339          4.7142          5.2752
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              377:        0.96402E-01

===============================================================


 INSTANT    0.378000000E+03   TIME STEP NUMBER             378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002928E+04
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 :  0.23763E+00 0.13253E+01
   Friction velocity        uet   :  0.14224E-01 0.79003E-01
   Friction velocity        uk    :  0.17497E-01 0.38742E-01
   Dimensionless distance   yplus :  0.42992E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57726E+01      55   0.13798E-02   0.18941E-01 
c  VelocityX    0.46299E+04      12   0.66460E-02   0.36797E-03 
c  VelocityY    0.46299E+04      12   0.66460E-02   0.22428E-04 
c  VelocityZ    0.46299E+04      12   0.66460E-02   0.36362E-04 
c  TurbEner     0.59783E+01      13   0.14307E-03   0.14419E-08 
c  Dissip       0.15003E+01      16   0.23662E-02   0.58817E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -165.17           54550           26777           27272
v  Velocity[x]             0.2925          2.0309         0.90805         0.90982
v  Velocity[y]           -0.38268         0.69162      0.00054896      0.00032889
v  Velocity[z]           -0.42279         0.51205      -0.0012642      -0.0013848
v  TurbEner             0.0010157        0.015487       0.0032864       0.0033459
v  Dissip              9.2167e-05        0.032227      0.00045183       0.0003906
v  TurbVisc               0.16622          11.345           4.714          5.2751
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              378:        0.94859E-01

===============================================================


 INSTANT    0.379000000E+03   TIME STEP NUMBER             379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999537E+04
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 :  0.23779E+00 0.12248E+01
   Friction velocity        uet   :  0.14233E-01 0.72601E-01
   Friction velocity        uk    :  0.17456E-01 0.38704E-01
   Dimensionless distance   yplus :  0.42923E+03 0.95177E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57461E+01      53   0.11715E-02   0.18835E-01 
c  VelocityX    0.46298E+04      12   0.65190E-02   0.28806E-03 
c  VelocityY    0.46298E+04      12   0.65190E-02   0.30919E-04 
c  VelocityZ    0.46298E+04      12   0.65190E-02   0.32335E-04 
c  TurbEner     0.59771E+01      13   0.13223E-03   0.16477E-08 
c  Dissip       0.14711E+01      16   0.19470E-02   0.53293E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.03           54556           26777           27272
v  Velocity[x]            0.29279           2.098         0.90805         0.90982
v  Velocity[y]           -0.36804         0.70067       0.0005424      0.00032065
v  Velocity[z]            -0.4204         0.50503       -0.001265      -0.0013835
v  TurbEner             0.0010176        0.014902       0.0032862       0.0033458
v  Dissip              9.2208e-05        0.030936      0.00045163      0.00039046
v  TurbVisc               0.16565          11.382          4.7139           5.275
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              379:        0.95374E-01

===============================================================


 INSTANT    0.380000000E+03   TIME STEP NUMBER             380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999407E+04
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 :  0.23753E+00 0.13236E+01
   Friction velocity        uet   :  0.14218E-01 0.78886E-01
   Friction velocity        uk    :  0.17472E-01 0.38707E-01
   Dimensionless distance   yplus :  0.42877E+03 0.95207E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64916E+01      61   0.14200E-02   0.21275E-01 
c  VelocityX    0.46299E+04      12   0.76279E-02   0.35827E-03 
c  VelocityY    0.46299E+04      12   0.76279E-02   0.33498E-04 
c  VelocityZ    0.46299E+04      12   0.76279E-02   0.30436E-04 
c  TurbEner     0.59778E+01      13   0.59194E-04   0.69297E-09 
c  Dissip       0.14849E+01      13   0.29212E-03   0.21528E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.97           54545           26777           27272
v  Velocity[x]            0.29303          2.1566         0.90806         0.90984
v  Velocity[y]           -0.38262         0.69467      0.00054692      0.00032754
v  Velocity[z]           -0.42103         0.51223      -0.0012541      -0.0013745
v  TurbEner             0.0010175        0.014824       0.0032862       0.0033458
v  Dissip               9.223e-05        0.030854      0.00045168      0.00039049
v  TurbVisc                0.1654          11.363          4.7137          5.2748
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              380:        0.97245E-01

===============================================================


 INSTANT    0.381000000E+03   TIME STEP NUMBER             381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999894E+04
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 :  0.23751E+00 0.12163E+01
   Friction velocity        uet   :  0.14216E-01 0.72506E-01
   Friction velocity        uk    :  0.17472E-01 0.38735E-01
   Dimensionless distance   yplus :  0.42920E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65996E+01      56   0.15154E-02   0.21626E-01 
c  VelocityX    0.46300E+04      12   0.73888E-02   0.44707E-03 
c  VelocityY    0.46300E+04      12   0.73888E-02   0.28239E-04 
c  VelocityZ    0.46300E+04      12   0.73888E-02   0.34943E-04 
c  TurbEner     0.59786E+01      13   0.79548E-04   0.13275E-08 
c  Dissip       0.15067E+01      15   0.92212E-03   0.20156E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.28           54520           26777           27271
v  Velocity[x]            0.29233          2.1825         0.90808         0.90985
v  Velocity[y]            -0.3667         0.70273      0.00054561      0.00032778
v  Velocity[z]           -0.42083         0.50637      -0.0012554      -0.0013737
v  TurbEner             0.0010142        0.014946       0.0032862       0.0033458
v  Dissip              9.2239e-05        0.031203      0.00045192      0.00039067
v  TurbVisc               0.16557          11.361          4.7136          5.2747
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              381:        0.95764E-01

===============================================================


 INSTANT    0.382000000E+03   TIME STEP NUMBER             382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001984E+04
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 :  0.23812E+00 0.13241E+01
   Friction velocity        uet   :  0.14251E-01 0.78927E-01
   Friction velocity        uk    :  0.17443E-01 0.38762E-01
   Dimensionless distance   yplus :  0.42890E+03 0.95182E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63969E+01      60   0.13736E-02   0.20978E-01 
c  VelocityX    0.46299E+04      12   0.67276E-02   0.42681E-03 
c  VelocityY    0.46299E+04      12   0.67276E-02   0.38724E-04 
c  VelocityZ    0.46299E+04      12   0.67276E-02   0.63722E-04 
c  TurbEner     0.59785E+01      13   0.12620E-03   0.15894E-08 
c  Dissip       0.15200E+01      16   0.21381E-02   0.48895E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.83           54528           26777           27271
v  Velocity[x]            0.29293          2.0155         0.90806         0.90983
v  Velocity[y]           -0.38232         0.69463      0.00053721       0.0003174
v  Velocity[z]           -0.42174         0.51133       -0.001261      -0.0013819
v  TurbEner             0.0010144        0.015572       0.0032864        0.003346
v  Dissip              9.2173e-05        0.032894      0.00045216      0.00039084
v  TurbVisc                0.1652          11.335          4.7134          5.2745
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              382:        0.96143E-01

===============================================================


 INSTANT    0.383000000E+03   TIME STEP NUMBER             383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999832E+04
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 :  0.23764E+00 0.12381E+01
   Friction velocity        uet   :  0.14222E-01 0.72537E-01
   Friction velocity        uk    :  0.17445E-01 0.38765E-01
   Dimensionless distance   yplus :  0.42809E+03 0.95180E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56347E+01      54   0.12119E-02   0.18462E-01 
c  VelocityX    0.46298E+04      13   0.69537E-02   0.40210E-03 
c  VelocityY    0.46298E+04      13   0.69537E-02   0.27958E-04 
c  VelocityZ    0.46298E+04      13   0.69537E-02   0.50613E-04 
c  TurbEner     0.59774E+01      14   0.14729E-03   0.20141E-08 
c  Dissip       0.14892E+01      16   0.23261E-02   0.68494E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.32           54525           26777           27271
v  Velocity[x]            0.29317           2.098         0.90807         0.90984
v  Velocity[y]             -0.367         0.70071      0.00054101      0.00031888
v  Velocity[z]           -0.42173         0.50488      -0.0012609      -0.0013779
v  TurbEner             0.0010158        0.014887       0.0032863       0.0033458
v  Dissip              9.2124e-05        0.031267      0.00045198      0.00039071
v  TurbVisc               0.16481          11.324          4.7134          5.2745
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              383:        0.94964E-01

===============================================================


 INSTANT    0.384000000E+03   TIME STEP NUMBER             384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998316E+04
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 :  0.23765E+00 0.13255E+01
   Friction velocity        uet   :  0.14221E-01 0.79003E-01
   Friction velocity        uk    :  0.17457E-01 0.38775E-01
   Dimensionless distance   yplus :  0.42890E+03 0.95172E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68691E+01      56   0.16028E-02   0.22534E-01 
c  VelocityX    0.46299E+04      12   0.62886E-02   0.36175E-03 
c  VelocityY    0.46299E+04      12   0.62886E-02   0.24137E-04 
c  VelocityZ    0.46299E+04      12   0.62886E-02   0.84738E-04 
c  TurbEner     0.59778E+01      12   0.64616E-04   0.82016E-09 
c  Dissip       0.14934E+01      13   0.54883E-03   0.34938E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.56           54531           26778           27272
v  Velocity[x]            0.29261          2.1621         0.90807         0.90984
v  Velocity[y]           -0.38243         0.69269       0.0005515      0.00033038
v  Velocity[z]           -0.42184         0.51192      -0.0012433      -0.0013615
v  TurbEner              0.001011        0.014754       0.0032864       0.0033459
v  Dissip              9.2097e-05        0.030882      0.00045203      0.00039075
v  TurbVisc               0.16523          11.351          4.7132          5.2744
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              384:        0.95884E-01

===============================================================


 INSTANT    0.385000000E+03   TIME STEP NUMBER             385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998542E+04
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 :  0.23771E+00 0.12153E+01
   Friction velocity        uet   :  0.14224E-01 0.72441E-01
   Friction velocity        uk    :  0.17416E-01 0.38674E-01
   Dimensionless distance   yplus :  0.42823E+03 0.95130E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66652E+01      55   0.13424E-02   0.21853E-01 
c  VelocityX    0.46299E+04      12   0.71996E-02   0.33339E-03 
c  VelocityY    0.46299E+04      12   0.71996E-02   0.38469E-04 
c  VelocityZ    0.46299E+04      12   0.71996E-02   0.42141E-04 
c  TurbEner     0.59777E+01      14   0.86710E-04   0.17427E-08 
c  Dissip       0.15087E+01      15   0.81934E-03   0.16095E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.26           54520           26778           27272
v  Velocity[x]            0.29247          2.1771         0.90806         0.90984
v  Velocity[y]           -0.36691         0.70084      0.00055311      0.00032919
v  Velocity[z]           -0.42093         0.50583      -0.0012563      -0.0013755
v  TurbEner              0.001013         0.01496       0.0032863       0.0033458
v  Dissip              9.2082e-05        0.031231      0.00045216      0.00039082
v  TurbVisc               0.16471          11.398          4.7132          5.2743
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              385:        0.95522E-01

===============================================================


 INSTANT    0.386000000E+03   TIME STEP NUMBER             386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001104E+04
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 :  0.23738E+00 0.13228E+01
   Friction velocity        uet   :  0.14203E-01 0.78849E-01
   Friction velocity        uk    :  0.17433E-01 0.38688E-01
   Dimensionless distance   yplus :  0.42781E+03 0.95146E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66999E+01      55   0.14135E-02   0.21967E-01 
c  VelocityX    0.46300E+04      12   0.73227E-02   0.36920E-03 
c  VelocityY    0.46300E+04      12   0.73227E-02   0.38931E-04 
c  VelocityZ    0.46300E+04      12   0.73227E-02   0.28002E-04 
c  TurbEner     0.59788E+01      13   0.75405E-04   0.91488E-09 
c  Dissip       0.15363E+01      15   0.88095E-03   0.14548E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.7           54526           26778           27272
v  Velocity[x]            0.29315          2.2148         0.90805         0.90983
v  Velocity[y]            -0.3828         0.69391      0.00055212      0.00033154
v  Velocity[z]           -0.41967         0.51055      -0.0012421      -0.0013633
v  TurbEner             0.0010129        0.015148       0.0032863       0.0033457
v  Dissip              9.2051e-05        0.031766      0.00045236      0.00039094
v  TurbVisc               0.16456          11.383           4.713          5.2742
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              386:        0.95579E-01

===============================================================


 INSTANT    0.387000000E+03   TIME STEP NUMBER             387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001463E+04
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 :  0.23798E+00 0.12159E+01
   Friction velocity        uet   :  0.14237E-01 0.72489E-01
   Friction velocity        uk    :  0.17432E-01 0.38718E-01
   Dimensionless distance   yplus :  0.42820E+03 0.95130E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63859E+01      62   0.16228E-02   0.20941E-01 
c  VelocityX    0.46298E+04      13   0.64859E-02   0.41946E-03 
c  VelocityY    0.46298E+04      13   0.64859E-02   0.36409E-04 
c  VelocityZ    0.46298E+04      13   0.64859E-02   0.46719E-04 
c  TurbEner     0.59792E+01      13   0.14028E-03   0.17168E-08 
c  Dissip       0.15567E+01      16   0.23802E-02   0.64873E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.8           54502           26777           27271
v  Velocity[x]            0.29289          2.0336         0.90807         0.90985
v  Velocity[y]           -0.36736         0.70086      0.00054939      0.00032958
v  Velocity[z]           -0.42204         0.50442      -0.0012476      -0.0013678
v  TurbEner             0.0010103        0.015818       0.0032863       0.0033457
v  Dissip              9.2002e-05        0.033667      0.00045262      0.00039114
v  TurbVisc               0.16481          11.331          4.7129          5.2741
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              387:        0.97112E-01

===============================================================


 INSTANT    0.388000000E+03   TIME STEP NUMBER             388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002009E+04
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 :  0.23781E+00 0.13249E+01
   Friction velocity        uet   :  0.14225E-01 0.78973E-01
   Friction velocity        uk    :  0.17410E-01 0.38755E-01
   Dimensionless distance   yplus :  0.42805E+03 0.95118E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64195E+01      62   0.13651E-02   0.21047E-01 
c  VelocityX    0.46299E+04      12   0.67001E-02   0.36079E-03 
c  VelocityY    0.46299E+04      12   0.67001E-02   0.40255E-04 
c  VelocityZ    0.46299E+04      12   0.67001E-02   0.11224E-03 
c  TurbEner     0.59776E+01      14   0.13081E-03   0.21832E-08 
c  Dissip       0.15359E+01      16   0.18032E-02   0.52545E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.29           54523           26776           27271
v  Velocity[x]            0.29253          2.1118         0.90804         0.90981
v  Velocity[y]           -0.38221         0.69442      0.00056192      0.00034001
v  Velocity[z]           -0.42314         0.51197      -0.0012429      -0.0013692
v  TurbEner             0.0010112        0.015276        0.003286       0.0033455
v  Dissip              9.2019e-05        0.032523      0.00045247      0.00039102
v  TurbVisc               0.16465          11.321          4.7127          5.2739
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              388:        0.96882E-01

===============================================================


 INSTANT    0.389000000E+03   TIME STEP NUMBER             389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001735E+04
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 :  0.23772E+00 0.12145E+01
   Friction velocity        uet   :  0.14219E-01 0.72329E-01
   Friction velocity        uk    :  0.17417E-01 0.38786E-01
   Dimensionless distance   yplus :  0.42747E+03 0.95160E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59277E+01      55   0.14253E-02   0.19423E-01 
c  VelocityX    0.46299E+04      12   0.71563E-02   0.36419E-03 
c  VelocityY    0.46299E+04      12   0.71563E-02   0.33909E-04 
c  VelocityZ    0.46299E+04      12   0.71563E-02   0.53063E-04 
c  TurbEner     0.59774E+01      12   0.65325E-04   0.61311E-09 
c  Dissip       0.15390E+01      13   0.44747E-03   0.34517E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.15           54515           26776           27270
v  Velocity[x]            0.29286           2.159         0.90807         0.90984
v  Velocity[y]           -0.36609         0.70266      0.00055614      0.00033224
v  Velocity[z]           -0.41987         0.50652      -0.0012497      -0.0013683
v  TurbEner             0.0010129        0.015136       0.0032858       0.0033453
v  Dissip              9.1993e-05        0.032281      0.00045245        0.000391
v  TurbVisc               0.16439          11.348          4.7126          5.2738
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              389:        0.95391E-01

===============================================================


 INSTANT    0.390000000E+03   TIME STEP NUMBER             390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002204E+04
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 :  0.23771E+00 0.13252E+01
   Friction velocity        uet   :  0.14217E-01 0.78999E-01
   Friction velocity        uk    :  0.17432E-01 0.38714E-01
   Dimensionless distance   yplus :  0.42838E+03 0.95151E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62331E+01      54   0.14767E-02   0.20438E-01 
c  VelocityX    0.46299E+04      12   0.69735E-02   0.37632E-03 
c  VelocityY    0.46299E+04      12   0.69735E-02   0.26386E-04 
c  VelocityZ    0.46299E+04      12   0.69735E-02   0.33829E-04 
c  TurbEner     0.59784E+01      13   0.74422E-04   0.93507E-09 
c  Dissip       0.15624E+01      15   0.82186E-03   0.16315E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.81           54510           26776           27270
v  Velocity[x]             0.2929          2.1945         0.90805         0.90983
v  Velocity[y]           -0.38227          0.6927      0.00055473      0.00033525
v  Velocity[z]            -0.4216          0.5111      -0.0012402      -0.0013613
v  TurbEner             0.0010085         0.01519       0.0032859       0.0033454
v  Dissip              9.1999e-05        0.032573       0.0004527      0.00039117
v  TurbVisc               0.16491          11.329          4.7124          5.2736
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              390:        0.95668E-01

===============================================================


 INSTANT    0.391000000E+03   TIME STEP NUMBER             391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000218E+04
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 :  0.23775E+00 0.12166E+01
   Friction velocity        uet   :  0.14219E-01 0.72521E-01
   Friction velocity        uk    :  0.17394E-01 0.38647E-01
   Dimensionless distance   yplus :  0.42780E+03 0.95210E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64102E+01      55   0.13990E-02   0.21012E-01 
c  VelocityX    0.46298E+04      12   0.65860E-02   0.40471E-03 
c  VelocityY    0.46298E+04      12   0.65860E-02   0.39133E-04 
c  VelocityZ    0.46298E+04      12   0.65860E-02   0.40103E-04 
c  TurbEner     0.59780E+01      13   0.11912E-03   0.14530E-08 
c  Dissip       0.15751E+01      16   0.19959E-02   0.44635E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.12           54506           26776           27270
v  Velocity[x]            0.29269          2.0172         0.90805         0.90982
v  Velocity[y]           -0.36775         0.70108      0.00054898      0.00032599
v  Velocity[z]           -0.42039         0.50415      -0.0012612      -0.0013787
v  TurbEner             0.0010104        0.015723       0.0032859       0.0033453
v  Dissip              9.1978e-05        0.034153      0.00045285      0.00039128
v  TurbVisc               0.16443          11.344          4.7123          5.2736
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              391:        0.95792E-01

===============================================================


 INSTANT    0.392000000E+03   TIME STEP NUMBER             392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000915E+04
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 :  0.23811E+00 0.13242E+01
   Friction velocity        uet   :  0.14240E-01 0.78935E-01
   Friction velocity        uk    :  0.17410E-01 0.38668E-01
   Dimensionless distance   yplus :  0.42743E+03 0.95257E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65304E+01      53   0.15186E-02   0.21418E-01 
c  VelocityX    0.46298E+04      12   0.65587E-02   0.31867E-03 
c  VelocityY    0.46298E+04      12   0.65587E-02   0.48954E-04 
c  VelocityZ    0.46298E+04      12   0.65587E-02   0.11465E-03 
c  TurbEner     0.59768E+01      14   0.14453E-03   0.21594E-08 
c  Dissip       0.15429E+01      16   0.22642E-02   0.75621E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.65           54516           26776           27270
v  Velocity[x]            0.29282          2.1005         0.90803         0.90981
v  Velocity[y]           -0.38244         0.69362      0.00055781      0.00033405
v  Velocity[z]             -0.421         0.51173      -0.0012412      -0.0013636
v  TurbEner             0.0010101        0.015096       0.0032857       0.0033452
v  Dissip              9.2031e-05        0.032674      0.00045264      0.00039113
v  TurbVisc               0.16437          11.311          4.7122          5.2735
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              392:        0.95575E-01

===============================================================


 INSTANT    0.393000000E+03   TIME STEP NUMBER             393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998953E+04
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 :  0.23765E+00 0.12171E+01
   Friction velocity        uet   :  0.14213E-01 0.72558E-01
   Friction velocity        uk    :  0.17408E-01 0.38734E-01
   Dimensionless distance   yplus :  0.42785E+03 0.95246E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62013E+01      67   0.15326E-02   0.20339E-01 
c  VelocityX    0.46298E+04      12   0.71428E-02   0.35310E-03 
c  VelocityY    0.46298E+04      12   0.71428E-02   0.34927E-04 
c  VelocityZ    0.46298E+04      12   0.71428E-02   0.52363E-04 
c  TurbEner     0.59763E+01      13   0.78907E-04   0.10411E-08 
c  Dissip       0.15403E+01      14   0.70165E-03   0.61942E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.76           54512           26777           27271
v  Velocity[x]            0.29275            2.15         0.90807         0.90985
v  Velocity[y]           -0.36659         0.70138      0.00055048      0.00032841
v  Velocity[z]           -0.42238         0.50599      -0.0012467       -0.001365
v  TurbEner             0.0010064        0.014926       0.0032854        0.003345
v  Dissip              9.2054e-05        0.032199      0.00045257      0.00039109
v  TurbVisc               0.16465          11.309          4.7121          5.2734
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              393:        0.98550E-01

===============================================================


 INSTANT    0.394000000E+03   TIME STEP NUMBER             394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999310E+04
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 :  0.23767E+00 0.13240E+01
   Friction velocity        uet   :  0.14215E-01 0.78917E-01
   Friction velocity        uk    :  0.17376E-01 0.38778E-01
   Dimensionless distance   yplus :  0.42742E+03 0.95315E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60768E+01      61   0.11309E-02   0.19915E-01 
c  VelocityX    0.46299E+04      12   0.73063E-02   0.38404E-03 
c  VelocityY    0.46299E+04      12   0.73063E-02   0.22858E-04 
c  VelocityZ    0.46299E+04      12   0.73063E-02   0.30277E-04 
c  TurbEner     0.59765E+01      12   0.63153E-04   0.77908E-09 
c  Dissip       0.15543E+01      14   0.59266E-03   0.89556E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.68           54513           26777           27271
v  Velocity[x]            0.29285          2.1881         0.90804         0.90981
v  Velocity[y]           -0.38226         0.69393      0.00055018      0.00033035
v  Velocity[z]           -0.42023           0.511      -0.0012476      -0.0013701
v  TurbEner             0.0010073        0.014966       0.0032853       0.0033449
v  Dissip              9.2071e-05        0.032284      0.00045262       0.0003911
v  TurbVisc               0.16433           11.34          4.7119          5.2732
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              394:        0.96492E-01

===============================================================


 INSTANT    0.395000000E+03   TIME STEP NUMBER             395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999573E+04
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 :  0.23762E+00 0.12162E+01
   Friction velocity        uet   :  0.14212E-01 0.72499E-01
   Friction velocity        uk    :  0.17384E-01 0.38720E-01
   Dimensionless distance   yplus :  0.42670E+03 0.95337E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65056E+01      54   0.15608E-02   0.21322E-01 
c  VelocityX    0.46297E+04      13   0.74287E-02   0.41048E-03 
c  VelocityY    0.46297E+04      13   0.74287E-02   0.47649E-04 
c  VelocityZ    0.46297E+04      13   0.74287E-02   0.37715E-04 
c  TurbEner     0.59767E+01      13   0.11380E-03   0.11479E-08 
c  Dissip       0.15622E+01      15   0.17392E-02   0.31790E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.66           54512           26776           27271
v  Velocity[x]            0.29304          2.0139         0.90805         0.90983
v  Velocity[y]           -0.36695         0.70167      0.00055361      0.00033208
v  Velocity[z]           -0.42102         0.50478      -0.0012586      -0.0013755
v  TurbEner             0.0010092        0.015499       0.0032851       0.0033448
v  Dissip              9.2094e-05        0.033652      0.00045268      0.00039115
v  TurbVisc                0.1641          11.325          4.7119          5.2732
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              395:        0.95792E-01

===============================================================


 INSTANT    0.396000000E+03   TIME STEP NUMBER             396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999836E+04
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 :  0.23772E+00 0.13251E+01
   Friction velocity        uet   :  0.14219E-01 0.78981E-01
   Friction velocity        uk    :  0.17400E-01 0.38727E-01
   Dimensionless distance   yplus :  0.42757E+03 0.95336E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62604E+01      54   0.15168E-02   0.20529E-01 
c  VelocityX    0.46298E+04      13   0.68124E-02   0.34754E-03 
c  VelocityY    0.46298E+04      13   0.68124E-02   0.25083E-04 
c  VelocityZ    0.46298E+04      13   0.68124E-02   0.98068E-04 
c  TurbEner     0.59757E+01      14   0.14442E-03   0.23063E-08 
c  Dissip       0.15206E+01      17   0.24390E-02   0.87258E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.7           54513           26777           27271
v  Velocity[x]            0.29252          2.0971         0.90804         0.90982
v  Velocity[y]           -0.38239         0.69534      0.00055574      0.00033751
v  Velocity[z]           -0.42233         0.51178      -0.0012375      -0.0013578
v  TurbEner             0.0010057        0.014896        0.003285       0.0033447
v  Dissip              9.2112e-05          0.0321      0.00045241      0.00039098
v  TurbVisc               0.16465          11.318          4.7118          5.2731
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              396:        0.96345E-01

===============================================================


 INSTANT    0.397000000E+03   TIME STEP NUMBER             397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999588E+04
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 :  0.23780E+00 0.12140E+01
   Friction velocity        uet   :  0.14225E-01 0.72345E-01
   Friction velocity        uk    :  0.17370E-01 0.38671E-01
   Dimensionless distance   yplus :  0.42716E+03 0.95359E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63845E+01      57   0.12345E-02   0.20927E-01 
c  VelocityX    0.46298E+04      12   0.70661E-02   0.41561E-03 
c  VelocityY    0.46298E+04      12   0.70661E-02   0.28953E-04 
c  VelocityZ    0.46298E+04      12   0.70661E-02   0.49496E-04 
c  TurbEner     0.59751E+01      12   0.67788E-04   0.82529E-09 
c  Dissip       0.15201E+01      14   0.57526E-03   0.47517E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.58           54504           26776           27270
v  Velocity[x]            0.29271          2.1472         0.90806         0.90984
v  Velocity[y]           -0.36684          0.7028      0.00055182      0.00032807
v  Velocity[z]           -0.42151         0.50574      -0.0012528      -0.0013722
v  TurbEner             0.0010088        0.014773       0.0032848       0.0033446
v  Dissip              9.2107e-05        0.031742      0.00045225      0.00039086
v  TurbVisc               0.16439          11.354          4.7117           5.273
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              397:        0.95787E-01

===============================================================


 INSTANT    0.398000000E+03   TIME STEP NUMBER             398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002328E+04
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 :  0.23782E+00 0.13257E+01
   Friction velocity        uet   :  0.14227E-01 0.79022E-01
   Friction velocity        uk    :  0.17396E-01 0.38740E-01
   Dimensionless distance   yplus :  0.42706E+03 0.95360E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66467E+01      58   0.14264E-02   0.21775E-01 
c  VelocityX    0.46299E+04      12   0.71910E-02   0.37307E-03 
c  VelocityY    0.46299E+04      12   0.71910E-02   0.32214E-04 
c  VelocityZ    0.46299E+04      12   0.71910E-02   0.37586E-04 
c  TurbEner     0.59761E+01      12   0.69055E-04   0.73243E-09 
c  Dissip       0.15380E+01      15   0.67309E-03   0.10751E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.77           54512           26776           27270
v  Velocity[x]            0.29269          2.1861         0.90806         0.90984
v  Velocity[y]           -0.38276         0.69264      0.00054798      0.00032832
v  Velocity[z]           -0.42066         0.51051      -0.0012539      -0.0013737
v  TurbEner             0.0010097        0.014833       0.0032847       0.0033445
v  Dissip                9.21e-05        0.031923      0.00045232       0.0003909
v  TurbVisc               0.16439          11.343          4.7117           5.273
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              398:        0.96052E-01

===============================================================


 INSTANT    0.399000000E+03   TIME STEP NUMBER             399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000593E+04
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 :  0.23777E+00 0.12171E+01
   Friction velocity        uet   :  0.14226E-01 0.72551E-01
   Friction velocity        uk    :  0.17404E-01 0.38807E-01
   Dimensionless distance   yplus :  0.42767E+03 0.95332E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67305E+01      56   0.16687E-02   0.22072E-01 
c  VelocityX    0.46298E+04      12   0.75368E-02   0.42873E-03 
c  VelocityY    0.46298E+04      12   0.75368E-02   0.40637E-04 
c  VelocityZ    0.46298E+04      12   0.75368E-02   0.41319E-04 
c  TurbEner     0.59765E+01      13   0.12137E-03   0.15806E-08 
c  Dissip       0.15486E+01      16   0.18104E-02   0.34886E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.4           54498           26775           27270
v  Velocity[x]             0.2928          2.0141         0.90807         0.90984
v  Velocity[y]           -0.36731         0.70056      0.00055485      0.00033421
v  Velocity[z]           -0.42121          0.5043      -0.0012644      -0.0013797
v  TurbEner             0.0010069        0.015369       0.0032848       0.0033445
v  Dissip              9.2115e-05        0.033331      0.00045242      0.00039098
v  TurbVisc               0.16472          11.355          4.7117           5.273
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              399:        0.96037E-01

===============================================================


 INSTANT    0.400000000E+03   TIME STEP NUMBER             400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000283E+04
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 :  0.23784E+00 0.13241E+01
   Friction velocity        uet   :  0.14231E-01 0.78929E-01
   Friction velocity        uk    :  0.17380E-01 0.38828E-01
   Dimensionless distance   yplus :  0.42748E+03 0.95331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63261E+01      57   0.13509E-02   0.20730E-01 
c  VelocityX    0.46297E+04      12   0.68771E-02   0.40900E-03 
c  VelocityY    0.46297E+04      12   0.68771E-02   0.27165E-04 
c  VelocityZ    0.46297E+04      12   0.68771E-02   0.94061E-04 
c  TurbEner     0.59750E+01      14   0.13874E-03   0.24489E-08 
c  Dissip       0.15096E+01      16   0.23488E-02   0.79023E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.87           54507           26775           27269
v  Velocity[x]            0.29283          2.0945         0.90806         0.90983
v  Velocity[y]           -0.38222         0.69602      0.00055085       0.0003295
v  Velocity[z]           -0.42153         0.51193      -0.0012502      -0.0013701
v  TurbEner             0.0010078         0.01479       0.0032847       0.0033445
v  Dissip              9.2089e-05        0.031835      0.00045213      0.00039078
v  TurbVisc               0.16441          11.335          4.7116          5.2729
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              400:        0.96220E-01

===============================================================


 INSTANT    0.401000000E+03   TIME STEP NUMBER             401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001517E+04
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 :  0.23762E+00 0.12132E+01
   Friction velocity        uet   :  0.14218E-01 0.72325E-01
   Friction velocity        uk    :  0.17388E-01 0.38818E-01
   Dimensionless distance   yplus :  0.42681E+03 0.95327E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57024E+01      56   0.13461E-02   0.18692E-01 
c  VelocityX    0.46298E+04      12   0.73329E-02   0.36614E-03 
c  VelocityY    0.46298E+04      12   0.73329E-02   0.28114E-04 
c  VelocityZ    0.46298E+04      12   0.73329E-02   0.49338E-04 
c  TurbEner     0.59753E+01      13   0.82012E-04   0.12380E-08 
c  Dissip       0.15111E+01      14   0.53362E-03   0.42495E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.42           54510           26775           27269
v  Velocity[x]            0.29287          2.1476         0.90806         0.90984
v  Velocity[y]           -0.36603         0.70411      0.00055084      0.00032672
v  Velocity[z]           -0.42014         0.50655      -0.0012521      -0.0013714
v  TurbEner             0.0010093        0.014681       0.0032847       0.0033444
v  Dissip              9.2076e-05         0.03152      0.00045201      0.00039069
v  TurbVisc               0.16412          11.329          4.7117          5.2729
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              401:        0.95659E-01

===============================================================


 INSTANT    0.402000000E+03   TIME STEP NUMBER             402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999820E+04
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 :  0.23730E+00 0.13254E+01
   Friction velocity        uet   :  0.14200E-01 0.79007E-01
   Friction velocity        uk    :  0.17401E-01 0.38689E-01
   Dimensionless distance   yplus :  0.42766E+03 0.95276E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62850E+01      54   0.15326E-02   0.20615E-01 
c  VelocityX    0.46298E+04      13   0.68992E-02   0.40429E-03 
c  VelocityY    0.46298E+04      13   0.68992E-02   0.24945E-04 
c  VelocityZ    0.46298E+04      13   0.68992E-02   0.34526E-04 
c  TurbEner     0.59760E+01      13   0.70889E-04   0.10491E-08 
c  Dissip       0.15312E+01      15   0.67880E-03   0.11253E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.01           54509           26776           27270
v  Velocity[x]            0.29255          2.1875         0.90806         0.90984
v  Velocity[y]           -0.38229         0.69162      0.00055219      0.00033198
v  Velocity[z]           -0.41988         0.51102      -0.0012353      -0.0013552
v  TurbEner             0.0010047        0.014733       0.0032846       0.0033444
v  Dissip              9.2052e-05        0.031695      0.00045209      0.00039075
v  TurbVisc               0.16456           11.36          4.7116          5.2729
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              402:        0.96168E-01

===============================================================


 INSTANT    0.403000000E+03   TIME STEP NUMBER             403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998632E+04
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 :  0.23769E+00 0.12184E+01
   Friction velocity        uet   :  0.14224E-01 0.72620E-01
   Friction velocity        uk    :  0.17361E-01 0.38684E-01
   Dimensionless distance   yplus :  0.42703E+03 0.95227E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60934E+01      57   0.13870E-02   0.19971E-01 
c  VelocityX    0.46298E+04      12   0.75939E-02   0.41381E-03 
c  VelocityY    0.46298E+04      12   0.75939E-02   0.25322E-04 
c  VelocityZ    0.46298E+04      12   0.75939E-02   0.48270E-04 
c  TurbEner     0.59756E+01      13   0.11423E-03   0.15678E-08 
c  Dissip       0.15395E+01      16   0.18447E-02   0.36824E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.75           54503           26775           27269
v  Velocity[x]            0.29281          2.0183         0.90805         0.90983
v  Velocity[y]           -0.36779         0.70046        0.000552      0.00032907
v  Velocity[z]           -0.42078         0.50417      -0.0012593       -0.001379
v  TurbEner             0.0010064        0.015251       0.0032845       0.0033443
v  Dissip              9.2071e-05        0.033115      0.00045216      0.00039081
v  TurbVisc                 0.164          11.346          4.7115          5.2728
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              403:        0.96009E-01

===============================================================


 INSTANT    0.404000000E+03   TIME STEP NUMBER             404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001385E+04
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 :  0.23746E+00 0.13236E+01
   Friction velocity        uet   :  0.14211E-01 0.78886E-01
   Friction velocity        uk    :  0.17376E-01 0.38762E-01
   Dimensionless distance   yplus :  0.42660E+03 0.95257E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63086E+01      59   0.14965E-02   0.20682E-01 
c  VelocityX    0.46297E+04      12   0.66441E-02   0.34707E-03 
c  VelocityY    0.46297E+04      12   0.66441E-02   0.57299E-04 
c  VelocityZ    0.46297E+04      12   0.66441E-02   0.12828E-03 
c  TurbEner     0.59743E+01      14   0.14254E-03   0.21448E-08 
c  Dissip       0.15018E+01      17   0.24165E-02   0.82621E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.66           54512           26775           27269
v  Velocity[x]            0.29294          2.0936         0.90804         0.90982
v  Velocity[y]           -0.38243         0.69379      0.00056261      0.00033985
v  Velocity[z]           -0.41915         0.51165      -0.0012388      -0.0013597
v  TurbEner             0.0010058        0.014667       0.0032842       0.0033441
v  Dissip              9.2054e-05        0.031592       0.0004518      0.00039056
v  TurbVisc               0.16389          11.351          4.7114          5.2727
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              404:        0.96289E-01

===============================================================


 INSTANT    0.405000000E+03   TIME STEP NUMBER             405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001357E+04
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 :  0.23784E+00 0.12167E+01
   Friction velocity        uet   :  0.14235E-01 0.72527E-01
   Friction velocity        uk    :  0.17371E-01 0.38790E-01
   Dimensionless distance   yplus :  0.42684E+03 0.95239E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59989E+01      64   0.13965E-02   0.19671E-01 
c  VelocityX    0.46298E+04      12   0.72464E-02   0.35060E-03 
c  VelocityY    0.46298E+04      12   0.72464E-02   0.32129E-04 
c  VelocityZ    0.46298E+04      12   0.72464E-02   0.58013E-04 
c  TurbEner     0.59745E+01      13   0.88360E-04   0.98650E-09 
c  Dissip       0.15040E+01      14   0.53749E-03   0.48570E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.52           54502           26775           27269
v  Velocity[x]            0.29256          2.1437         0.90806         0.90984
v  Velocity[y]           -0.36662         0.70178      0.00055662      0.00033635
v  Velocity[z]           -0.42109         0.50591      -0.0012481      -0.0013642
v  TurbEner             0.0010027        0.014596        0.003284        0.003344
v  Dissip              9.2062e-05        0.031313      0.00045167      0.00039047
v  TurbVisc               0.16402          11.329          4.7114          5.2727
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              405:        0.97917E-01

===============================================================


 INSTANT    0.406000000E+03   TIME STEP NUMBER             406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999677E+04
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 :  0.23747E+00 0.13238E+01
   Friction velocity        uet   :  0.14213E-01 0.78899E-01
   Friction velocity        uk    :  0.17344E-01 0.38763E-01
   Dimensionless distance   yplus :  0.42659E+03 0.95215E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63722E+01      58   0.12394E-02   0.20880E-01 
c  VelocityX    0.46298E+04      12   0.70342E-02   0.36459E-03 
c  VelocityY    0.46298E+04      12   0.70342E-02   0.25626E-04 
c  VelocityZ    0.46298E+04      12   0.70342E-02   0.37526E-04 
c  TurbEner     0.59744E+01      13   0.76178E-04   0.10332E-08 
c  Dissip       0.15209E+01      15   0.65154E-03   0.10287E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.34           54504           26775           27270
v  Velocity[x]            0.29274          2.1843         0.90805         0.90983
v  Velocity[y]            -0.3823         0.69402      0.00055298      0.00033362
v  Velocity[z]           -0.41961         0.51105      -0.0012461      -0.0013688
v  TurbEner             0.0010033        0.014657       0.0032838       0.0033439
v  Dissip              9.2101e-05        0.031471      0.00045171      0.00039049
v  TurbVisc               0.16369          11.325          4.7113          5.2726
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              406:        0.95629E-01

===============================================================


 INSTANT    0.407000000E+03   TIME STEP NUMBER             407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998566E+04
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 :  0.23719E+00 0.12161E+01
   Friction velocity        uet   :  0.14196E-01 0.72490E-01
   Friction velocity        uk    :  0.17349E-01 0.38741E-01
   Dimensionless distance   yplus :  0.42590E+03 0.95148E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57790E+01      54   0.14709E-02   0.18946E-01 
c  VelocityX    0.46298E+04      12   0.70741E-02   0.40548E-03 
c  VelocityY    0.46298E+04      12   0.70741E-02   0.24316E-04 
c  VelocityZ    0.46298E+04      12   0.70741E-02   0.47990E-04 
c  TurbEner     0.59748E+01      13   0.10929E-03   0.11489E-08 
c  Dissip       0.15281E+01      15   0.17714E-02   0.31971E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.25           54506           26775           27269
v  Velocity[x]            0.29305          2.0162         0.90806         0.90984
v  Velocity[y]           -0.36693         0.70104       0.0005484      0.00032811
v  Velocity[z]           -0.41937         0.50475      -0.0012644      -0.0013836
v  TurbEner             0.0010045        0.015169       0.0032839       0.0033439
v  Dissip              9.2155e-05        0.032838      0.00045179      0.00039056
v  TurbVisc               0.16345          11.354          4.7112          5.2725
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              407:        0.95253E-01

===============================================================


 INSTANT    0.408000000E+03   TIME STEP NUMBER             408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001870E+04
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 :  0.23777E+00 0.13251E+01
   Friction velocity        uet   :  0.14232E-01 0.78984E-01
   Friction velocity        uk    :  0.17359E-01 0.38758E-01
   Dimensionless distance   yplus :  0.42672E+03 0.95125E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71754E+01      56   0.16422E-02   0.23530E-01 
c  VelocityX    0.46297E+04      13   0.63746E-02   0.40333E-03 
c  VelocityY    0.46297E+04      13   0.63746E-02   0.45270E-04 
c  VelocityZ    0.46297E+04      13   0.63746E-02   0.12047E-03 
c  TurbEner     0.59738E+01      13   0.13848E-03   0.20280E-08 
c  Dissip       0.14905E+01      17   0.25186E-02   0.85556E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.7           54519           26775           27269
v  Velocity[x]            0.29247           2.096         0.90806         0.90983
v  Velocity[y]           -0.38241         0.69439      0.00056415      0.00034589
v  Velocity[z]           -0.41912         0.51176      -0.0012332      -0.0013564
v  TurbEner             0.0009995        0.014588       0.0032837       0.0033438
v  Dissip              9.2189e-05        0.031214      0.00045152      0.00039038
v  TurbVisc               0.16387          11.336          4.7113          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              408:        0.95944E-01

===============================================================


 INSTANT    0.409000000E+03   TIME STEP NUMBER             409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999339E+04
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 :  0.23776E+00 0.12133E+01
   Friction velocity        uet   :  0.14231E-01 0.72297E-01
   Friction velocity        uk    :  0.17316E-01 0.38704E-01
   Dimensionless distance   yplus :  0.42604E+03 0.95141E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70459E+01      57   0.14426E-02   0.23094E-01 
c  VelocityX    0.46297E+04      12   0.73757E-02   0.35677E-03 
c  VelocityY    0.46297E+04      12   0.73757E-02   0.64038E-04 
c  VelocityZ    0.46297E+04      12   0.73757E-02   0.59550E-04 
c  TurbEner     0.59734E+01      13   0.72755E-04   0.12011E-08 
c  Dissip       0.14817E+01      14   0.76352E-03   0.72495E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.88           54504           26775           27269
v  Velocity[x]            0.29275          2.1392         0.90806         0.90983
v  Velocity[y]           -0.36689         0.70269      0.00055074      0.00032782
v  Velocity[z]           -0.41888         0.50569      -0.0012491      -0.0013696
v  TurbEner              0.001001        0.014522       0.0032836       0.0033437
v  Dissip              9.2163e-05        0.030703       0.0004514      0.00039028
v  TurbVisc               0.16321          11.354          4.7113          5.2726
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              409:        0.95517E-01

===============================================================


 INSTANT    0.410000000E+03   TIME STEP NUMBER             410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998407E+04
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 :  0.23778E+00 0.13249E+01
   Friction velocity        uet   :  0.14233E-01 0.78978E-01
   Friction velocity        uk    :  0.17329E-01 0.38698E-01
   Dimensionless distance   yplus :  0.42557E+03 0.95161E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69425E+01      62   0.13328E-02   0.22751E-01 
c  VelocityX    0.46298E+04      12   0.66128E-02   0.36536E-03 
c  VelocityY    0.46298E+04      12   0.66128E-02   0.42666E-04 
c  VelocityZ    0.46298E+04      12   0.66128E-02   0.31469E-04 
c  TurbEner     0.59747E+01      13   0.74107E-04   0.10413E-08 
c  Dissip       0.14961E+01      14   0.53544E-03   0.66724E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.01           54519           26776           27270
v  Velocity[x]            0.29306          2.1844         0.90804         0.90982
v  Velocity[y]           -0.38282          0.6927      0.00055283      0.00033124
v  Velocity[z]           -0.42012         0.51038      -0.0012451      -0.0013676
v  TurbEner             0.0010004        0.014658       0.0032837       0.0033438
v  Dissip              9.2111e-05        0.030844      0.00045147      0.00039031
v  TurbVisc               0.16318          11.334          4.7113          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              410:        0.96059E-01

===============================================================


 INSTANT    0.411000000E+03   TIME STEP NUMBER             411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998664E+04
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 :  0.23786E+00 0.12170E+01
   Friction velocity        uet   :  0.14238E-01 0.72543E-01
   Friction velocity        uk    :  0.17324E-01 0.38694E-01
   Dimensionless distance   yplus :  0.42589E+03 0.95193E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62701E+01      62   0.14684E-02   0.20565E-01 
c  VelocityX    0.46297E+04      13   0.71224E-02   0.41147E-03 
c  VelocityY    0.46297E+04      13   0.71224E-02   0.36406E-04 
c  VelocityZ    0.46297E+04      13   0.71224E-02   0.45283E-04 
c  TurbEner     0.59750E+01      13   0.12768E-03   0.14352E-08 
c  Dissip       0.15060E+01      16   0.18967E-02   0.37481E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.68           54533           26776           27270
v  Velocity[x]             0.2926          2.0115         0.90806         0.90984
v  Velocity[y]           -0.36734         0.70029      0.00054461      0.00032263
v  Velocity[z]           -0.42068         0.50432      -0.0012613      -0.0013803
v  TurbEner            0.00099716        0.015273       0.0032837       0.0033437
v  Dissip              9.2093e-05        0.032307      0.00045154      0.00039037
v  TurbVisc               0.16338           11.34          4.7114          5.2727
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              411:        0.97614E-01

===============================================================


 INSTANT    0.412000000E+03   TIME STEP NUMBER             412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999962E+04
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 :  0.23774E+00 0.13246E+01
   Friction velocity        uet   :  0.14230E-01 0.78958E-01
   Friction velocity        uk    :  0.17296E-01 0.38721E-01
   Dimensionless distance   yplus :  0.42551E+03 0.95207E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60448E+01      56   0.13499E-02   0.19822E-01 
c  VelocityX    0.46297E+04      12   0.68400E-02   0.31355E-03 
c  VelocityY    0.46297E+04      12   0.68400E-02   0.34632E-04 
c  VelocityZ    0.46297E+04      12   0.68400E-02   0.10805E-03 
c  TurbEner     0.59742E+01      13   0.12486E-03   0.17338E-08 
c  Dissip       0.14732E+01      16   0.22076E-02   0.69814E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.25           54544           26776           27270
v  Velocity[x]            0.29266          2.0942         0.90803         0.90981
v  Velocity[y]           -0.38221          0.6934      0.00055323      0.00033199
v  Velocity[z]           -0.41993         0.51185      -0.0012426      -0.0013674
v  TurbEner            0.00099825        0.014756       0.0032836       0.0033437
v  Dissip              9.2099e-05         0.03091       0.0004513      0.00039021
v  TurbVisc               0.16303          11.317          4.7113          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              412:        0.95774E-01

===============================================================


 INSTANT    0.413000000E+03   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001333E+04
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 :  0.23776E+00 0.12165E+01
   Friction velocity        uet   :  0.14232E-01 0.72517E-01
   Friction velocity        uk    :  0.17305E-01 0.38739E-01
   Dimensionless distance   yplus :  0.42483E+03 0.95195E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65138E+01      58   0.15071E-02   0.21343E-01 
c  VelocityX    0.46298E+04      12   0.71096E-02   0.36508E-03 
c  VelocityY    0.46298E+04      12   0.71096E-02   0.38087E-04 
c  VelocityZ    0.46298E+04      12   0.71096E-02   0.53870E-04 
c  TurbEner     0.59742E+01      13   0.60718E-04   0.74027E-09 
c  Dissip       0.14714E+01      14   0.61101E-03   0.48078E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.09           54536           26775           27269
v  Velocity[x]            0.29328           2.145         0.90807         0.90985
v  Velocity[y]           -0.36607         0.70196      0.00054941      0.00032857
v  Velocity[z]           -0.42001         0.50648      -0.0012473      -0.0013648
v  TurbEner             0.0010006        0.014671       0.0032835       0.0033435
v  Dissip              9.2089e-05         0.03052      0.00045122      0.00039015
v  TurbVisc               0.16286          11.311          4.7113          5.2726
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              413:        0.95730E-01

===============================================================


 INSTANT    0.414000000E+03   TIME STEP NUMBER             414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000562E+04
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 :  0.23770E+00 0.13234E+01
   Friction velocity        uet   :  0.14228E-01 0.78886E-01
   Friction velocity        uk    :  0.17326E-01 0.38778E-01
   Dimensionless distance   yplus :  0.42579E+03 0.95226E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61738E+01      57   0.13903E-02   0.20242E-01 
c  VelocityX    0.46298E+04      12   0.66795E-02   0.37739E-03 
c  VelocityY    0.46298E+04      12   0.66795E-02   0.29923E-04 
c  VelocityZ    0.46298E+04      12   0.66795E-02   0.34418E-04 
c  TurbEner     0.59753E+01      13   0.83279E-04   0.12139E-08 
c  Dissip       0.14891E+01      15   0.68462E-03   0.11361E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.54           54513           26776           27270
v  Velocity[x]            0.29284           2.184         0.90807         0.90984
v  Velocity[y]           -0.38227         0.69471      0.00055491      0.00033699
v  Velocity[z]           -0.42139         0.51104       -0.001239        -0.00136
v  TurbEner            0.00099696         0.01479       0.0032837       0.0033437
v  Dissip              9.2051e-05        0.030719       0.0004514      0.00039027
v  TurbVisc               0.16343          11.341          4.7113          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              414:        0.96150E-01

===============================================================


 INSTANT    0.415000000E+03   TIME STEP NUMBER             415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998610E+04
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 :  0.23740E+00 0.12168E+01
   Friction velocity        uet   :  0.14210E-01 0.72536E-01
   Friction velocity        uk    :  0.17294E-01 0.38701E-01
   Dimensionless distance   yplus :  0.42531E+03 0.95280E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61520E+01      56   0.13810E-02   0.20180E-01 
c  VelocityX    0.46298E+04      13   0.67578E-02   0.37104E-03 
c  VelocityY    0.46298E+04      13   0.67578E-02   0.36512E-04 
c  VelocityZ    0.46298E+04      13   0.67578E-02   0.34486E-04 
c  TurbEner     0.59752E+01      13   0.11845E-03   0.15080E-08 
c  Dissip       0.14999E+01      16   0.19115E-02   0.39370E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.07           54521           26776           27270
v  Velocity[x]            0.29248          2.0099         0.90804         0.90982
v  Velocity[y]           -0.36766         0.70111      0.00055568       0.0003328
v  Velocity[z]           -0.41971         0.50421      -0.0012555      -0.0013725
v  TurbEner            0.00099923        0.015377       0.0032838       0.0033438
v  Dissip              9.1987e-05        0.032204      0.00045151      0.00039036
v  TurbVisc               0.16304           11.39          4.7113          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              415:        0.96129E-01

===============================================================


 INSTANT    0.416000000E+03   TIME STEP NUMBER             416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000518E+04
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 :  0.23782E+00 0.13259E+01
   Friction velocity        uet   :  0.14235E-01 0.79036E-01
   Friction velocity        uk    :  0.17314E-01 0.38718E-01
   Dimensionless distance   yplus :  0.42491E+03 0.95256E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62388E+01      58   0.12606E-02   0.20451E-01 
c  VelocityX    0.46297E+04      13   0.67521E-02   0.29726E-03 
c  VelocityY    0.46297E+04      13   0.67521E-02   0.37094E-04 
c  VelocityZ    0.46297E+04      13   0.67521E-02   0.57997E-04 
c  TurbEner     0.59741E+01      14   0.13217E-03   0.19694E-08 
c  Dissip       0.14691E+01      16   0.20783E-02   0.64311E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.72           54532           26776           27270
v  Velocity[x]            0.29269          2.0905         0.90802         0.90981
v  Velocity[y]           -0.38246         0.69472      0.00055358      0.00033231
v  Velocity[z]           -0.42038         0.51173      -0.0012478      -0.0013697
v  TurbEner             0.0010006        0.014836       0.0032836       0.0033436
v  Dissip              9.1977e-05        0.030901      0.00045127      0.00039019
v  TurbVisc               0.16294          11.378          4.7114          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              416:        0.96403E-01

===============================================================


 INSTANT    0.417000000E+03   TIME STEP NUMBER             417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999997E+04
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 :  0.23760E+00 0.12138E+01
   Friction velocity        uet   :  0.14223E-01 0.72326E-01
   Friction velocity        uk    :  0.17326E-01 0.38761E-01
   Dimensionless distance   yplus :  0.42562E+03 0.95244E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56912E+01      55   0.12789E-02   0.18659E-01 
c  VelocityX    0.46298E+04      12   0.63842E-02   0.30450E-03 
c  VelocityY    0.46298E+04      12   0.63842E-02   0.25254E-04 
c  VelocityZ    0.46298E+04      12   0.63842E-02   0.36982E-04 
c  TurbEner     0.59738E+01      12   0.60669E-04   0.50305E-09 
c  Dissip       0.14714E+01      14   0.57955E-03   0.42825E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.34           54539           26775           27270
v  Velocity[x]            0.29283          2.1416         0.90806         0.90983
v  Velocity[y]           -0.36615         0.70273      0.00054788      0.00032568
v  Velocity[z]           -0.41979         0.50636      -0.0012578      -0.0013759
v  TurbEner            0.00099817        0.014712       0.0032835       0.0033435
v  Dissip              9.1964e-05        0.030546      0.00045119      0.00039012
v  TurbVisc               0.16335          11.327          4.7113          5.2726
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              417:        0.95388E-01

===============================================================


 INSTANT    0.418000000E+03   TIME STEP NUMBER             418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001446E+04
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 :  0.23720E+00 0.13252E+01
   Friction velocity        uet   :  0.14198E-01 0.78993E-01
   Friction velocity        uk    :  0.17305E-01 0.38807E-01
   Dimensionless distance   yplus :  0.42549E+03 0.95273E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61135E+01      58   0.12212E-02   0.20035E-01 
c  VelocityX    0.46298E+04      12   0.73914E-02   0.32964E-03 
c  VelocityY    0.46298E+04      12   0.73914E-02   0.32554E-04 
c  VelocityZ    0.46298E+04      12   0.73914E-02   0.79588E-04 
c  TurbEner     0.59749E+01      12   0.64076E-04   0.71856E-09 
c  Dissip       0.14892E+01      15   0.65326E-03   0.10317E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.26           54549           26776           27270
v  Velocity[x]            0.29263          2.1841         0.90805         0.90983
v  Velocity[y]           -0.38239         0.69238      0.00054985      0.00032867
v  Velocity[z]           -0.41964         0.51082      -0.0012398      -0.0013613
v  TurbEner            0.00099985         0.01479       0.0032836       0.0033435
v  Dissip              9.1983e-05        0.030685       0.0004513      0.00039019
v  TurbVisc               0.16314          11.315          4.7113          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              418:        0.95960E-01

===============================================================


 INSTANT    0.419000000E+03   TIME STEP NUMBER             419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999488E+04
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 :  0.23785E+00 0.12544E+01
   Friction velocity        uet   :  0.14237E-01 0.73085E-01
   Friction velocity        uk    :  0.17319E-01 0.38817E-01
   Dimensionless distance   yplus :  0.42501E+03 0.95230E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59914E+01      53   0.14580E-02   0.19638E-01 
c  VelocityX    0.46297E+04      12   0.67474E-02   0.41901E-03 
c  VelocityY    0.46297E+04      12   0.67474E-02   0.27160E-04 
c  VelocityZ    0.46297E+04      12   0.67474E-02   0.40137E-04 
c  TurbEner     0.59753E+01      13   0.12060E-03   0.11736E-08 
c  Dissip       0.15019E+01      16   0.19896E-02   0.42637E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.74           54553           26776           27270
v  Velocity[x]            0.29308          2.0209         0.90805         0.90983
v  Velocity[y]           -0.36787         0.70006      0.00054807      0.00032488
v  Velocity[z]           -0.42007           0.504      -0.0012567      -0.0013743
v  TurbEner             0.0010026        0.015373       0.0032838       0.0033436
v  Dissip              9.1951e-05        0.032231      0.00045152      0.00039035
v  TurbVisc               0.16298          11.342          4.7113          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              419:        0.95119E-01

===============================================================


 INSTANT    0.420000000E+03   TIME STEP NUMBER             420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998342E+04
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 :  0.23768E+00 0.13246E+01
   Friction velocity        uet   :  0.14227E-01 0.78952E-01
   Friction velocity        uk    :  0.17343E-01 0.38786E-01
   Dimensionless distance   yplus :  0.42613E+03 0.95251E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60614E+01      55   0.14530E-02   0.19865E-01 
c  VelocityX    0.46298E+04      13   0.69912E-02   0.33160E-03 
c  VelocityY    0.46298E+04      13   0.69912E-02   0.25030E-04 
c  VelocityZ    0.46298E+04      13   0.69912E-02   0.51351E-04 
c  TurbEner     0.59744E+01      14   0.12900E-03   0.19242E-08 
c  Dissip       0.14703E+01      16   0.20648E-02   0.64612E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.1           54544           26776           27270
v  Velocity[x]            0.29262          2.0928         0.90806         0.90984
v  Velocity[y]             -0.383         0.69509      0.00054612      0.00032665
v  Velocity[z]              -0.42         0.51123      -0.0012471      -0.0013683
v  TurbEner            0.00099915        0.014823       0.0032837       0.0033436
v  Dissip              9.1974e-05         0.03095      0.00045129      0.00039019
v  TurbVisc                0.1636          11.324          4.7114          5.2726
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              420:        0.96245E-01

===============================================================


 INSTANT    0.421000000E+03   TIME STEP NUMBER             421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998612E+04
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 :  0.23777E+00 0.12133E+01
   Friction velocity        uet   :  0.14232E-01 0.72324E-01
   Friction velocity        uk    :  0.17313E-01 0.38663E-01
   Dimensionless distance   yplus :  0.42571E+03 0.95253E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67892E+01      63   0.16195E-02   0.22267E-01 
c  VelocityX    0.46299E+04      13   0.72259E-02   0.36736E-03 
c  VelocityY    0.46299E+04      13   0.72259E-02   0.27534E-04 
c  VelocityZ    0.46299E+04      13   0.72259E-02   0.52117E-04 
c  TurbEner     0.59747E+01      13   0.65104E-04   0.93658E-09 
c  Dissip       0.14736E+01      14   0.52729E-03   0.43540E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.19           54520           26777           27271
v  Velocity[x]             0.2927          2.1403         0.90807         0.90985
v  Velocity[y]           -0.36816         0.70371      0.00055759      0.00033736
v  Velocity[z]           -0.42059         0.50691      -0.0012524      -0.0013689
v  TurbEner             0.0010024        0.014716       0.0032838       0.0033437
v  Dissip              9.2006e-05        0.030643       0.0004513       0.0003902
v  TurbVisc               0.16326          11.331          4.7114          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              421:        0.97124E-01

===============================================================


 INSTANT    0.422000000E+03   TIME STEP NUMBER             422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998737E+04
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 :  0.23769E+00 0.13247E+01
   Friction velocity        uet   :  0.14226E-01 0.78963E-01
   Friction velocity        uk    :  0.17341E-01 0.38690E-01
   Dimensionless distance   yplus :  0.42559E+03 0.95236E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69473E+01      60   0.14285E-02   0.22759E-01 
c  VelocityX    0.46298E+04      12   0.75144E-02   0.35918E-03 
c  VelocityY    0.46298E+04      12   0.75144E-02   0.76096E-04 
c  VelocityZ    0.46298E+04      12   0.75144E-02   0.10734E-03 
c  TurbEner     0.59756E+01      13   0.75266E-04   0.14200E-08 
c  Dissip       0.14942E+01      15   0.69927E-03   0.12033E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -167.5           54529           26777           27271
v  Velocity[x]            0.29297          2.1832         0.90806         0.90983
v  Velocity[y]            -0.3828         0.69194      0.00055589      0.00033516
v  Velocity[z]            -0.4202         0.51377      -0.0012368      -0.0013561
v  TurbEner             0.0010036        0.014823       0.0032841       0.0033439
v  Dissip              9.2049e-05        0.030838      0.00045147      0.00039031
v  TurbVisc               0.16333          11.372          4.7115          5.2727
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              422:        0.95861E-01

===============================================================


 INSTANT    0.423000000E+03   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998983E+04
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 :  0.23725E+00 0.12393E+01
   Friction velocity        uet   :  0.14199E-01 0.72585E-01
   Friction velocity        uk    :  0.17352E-01 0.38734E-01
   Dimensionless distance   yplus :  0.42629E+03 0.95266E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62069E+01      60   0.13908E-02   0.20356E-01 
c  VelocityX    0.46298E+04      12   0.68194E-02   0.47098E-03 
c  VelocityY    0.46298E+04      12   0.68194E-02   0.34310E-04 
c  VelocityZ    0.46298E+04      12   0.68194E-02   0.49837E-04 
c  TurbEner     0.59762E+01      14   0.13120E-03   0.19899E-08 
c  Dissip       0.15081E+01      16   0.19751E-02   0.43907E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.54           54526           26777           27271
v  Velocity[x]            0.29261          2.0165         0.90807         0.90984
v  Velocity[y]           -0.36654         0.70074      0.00055573      0.00033249
v  Velocity[z]           -0.42047         0.50787      -0.0012551       -0.001373
v  TurbEner             0.0010023        0.015428       0.0032844       0.0033441
v  Dissip              9.2097e-05        0.032361      0.00045174       0.0003905
v  TurbVisc               0.16377          11.354          4.7116          5.2729
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              423:        0.96251E-01

===============================================================


 INSTANT    0.424000000E+03   TIME STEP NUMBER             424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001170E+04
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 :  0.23779E+00 0.13241E+01
   Friction velocity        uet   :  0.14230E-01 0.78918E-01
   Friction velocity        uk    :  0.17340E-01 0.38770E-01
   Dimensionless distance   yplus :  0.42635E+03 0.95276E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58924E+01      56   0.14961E-02   0.19324E-01 
c  VelocityX    0.46298E+04      12   0.67954E-02   0.41241E-03 
c  VelocityY    0.46298E+04      12   0.67954E-02   0.27282E-04 
c  VelocityZ    0.46298E+04      12   0.67954E-02   0.48082E-04 
c  TurbEner     0.59751E+01      13   0.13067E-03   0.18793E-08 
c  Dissip       0.14708E+01      16   0.22475E-02   0.73728E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.4           54506           26777           27271
v  Velocity[x]            0.29275          2.0931         0.90807         0.90984
v  Velocity[y]           -0.38269         0.69453      0.00055938      0.00033963
v  Velocity[z]           -0.41982         0.51217       -0.001244      -0.0013628
v  TurbEner             0.0010049        0.014855       0.0032844       0.0033441
v  Dissip              9.2121e-05        0.030929      0.00045152      0.00039035
v  TurbVisc               0.16379          11.358          4.7117           5.273
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              424:        0.95979E-01

===============================================================


 INSTANT    0.425000000E+03   TIME STEP NUMBER             425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999764E+04
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 :  0.23786E+00 0.12175E+01
   Friction velocity        uet   :  0.14233E-01 0.72583E-01
   Friction velocity        uk    :  0.17363E-01 0.38769E-01
   Dimensionless distance   yplus :  0.42600E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58357E+01      56   0.12047E-02   0.19125E-01 
c  VelocityX    0.46299E+04      12   0.66552E-02   0.37740E-03 
c  VelocityY    0.46299E+04      12   0.66552E-02   0.23886E-04 
c  VelocityZ    0.46299E+04      12   0.66552E-02   0.57768E-04 
c  TurbEner     0.59749E+01      13   0.64639E-04   0.10836E-08 
c  Dissip       0.14725E+01      14   0.52862E-03   0.43018E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.37           54515           26776           27271
v  Velocity[x]            0.29276          2.1409         0.90804         0.90982
v  Velocity[y]           -0.36821         0.70273      0.00055701      0.00033446
v  Velocity[z]           -0.41981         0.50494      -0.0012602      -0.0013782
v  TurbEner             0.0010081        0.014769       0.0032846       0.0033442
v  Dissip              9.2097e-05        0.030608      0.00045151      0.00039033
v  TurbVisc               0.16372          11.334          4.7117          5.2729
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              425:        0.10075E+00

===============================================================


 INSTANT    0.426000000E+03   TIME STEP NUMBER             426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001568E+04
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 :  0.23790E+00 0.13237E+01
   Friction velocity        uet   :  0.14234E-01 0.78902E-01
   Friction velocity        uk    :  0.17391E-01 0.38739E-01
   Dimensionless distance   yplus :  0.42712E+03 0.95263E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63845E+01      57   0.14605E-02   0.20933E-01 
c  VelocityX    0.46299E+04      12   0.72619E-02   0.31184E-03 
c  VelocityY    0.46299E+04      12   0.72619E-02   0.62342E-04 
c  VelocityZ    0.46299E+04      12   0.72619E-02   0.10607E-03 
c  TurbEner     0.59762E+01      13   0.76851E-04   0.98955E-09 
c  Dissip       0.14937E+01      15   0.70547E-03   0.11759E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.92           54521           26776           27271
v  Velocity[x]            0.29279          2.1825         0.90804         0.90983
v  Velocity[y]           -0.38251         0.69545        0.000561      0.00034234
v  Velocity[z]           -0.42126         0.51229      -0.0012366      -0.0013577
v  TurbEner             0.0010062        0.014897       0.0032846       0.0033443
v  Dissip              9.2082e-05        0.030836      0.00045163      0.00039041
v  TurbVisc               0.16442           11.33          4.7118          5.2731
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              426:        0.95447E-01

===============================================================


 INSTANT    0.427000000E+03   TIME STEP NUMBER             427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999782E+04
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 :  0.23778E+00 0.12172E+01
   Friction velocity        uet   :  0.14226E-01 0.72563E-01
   Friction velocity        uk    :  0.17374E-01 0.38652E-01
   Dimensionless distance   yplus :  0.42701E+03 0.95287E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60879E+01      65   0.15707E-02   0.19971E-01 
c  VelocityX    0.46298E+04      12   0.69525E-02   0.43174E-03 
c  VelocityY    0.46298E+04      12   0.69525E-02   0.24052E-04 
c  VelocityZ    0.46298E+04      12   0.69525E-02   0.51847E-04 
c  TurbEner     0.59767E+01      13   0.13005E-03   0.16328E-08 
c  Dissip       0.15085E+01      16   0.20083E-02   0.46183E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.1           54511           26776           27271
v  Velocity[x]             0.2929           2.017         0.90807         0.90984
v  Velocity[y]           -0.36621         0.70156      0.00056261      0.00034056
v  Velocity[z]           -0.42146         0.50686      -0.0012459      -0.0013653
v  TurbEner             0.0010107        0.015514       0.0032848       0.0033444
v  Dissip              9.2051e-05        0.032388      0.00045185      0.00039057
v  TurbVisc               0.16432          11.358          4.7118          5.2731
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              427:        0.97872E-01

===============================================================


 INSTANT    0.428000000E+03   TIME STEP NUMBER             428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000040E+04
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 :  0.23765E+00 0.13262E+01
   Friction velocity        uet   :  0.14217E-01 0.79047E-01
   Friction velocity        uk    :  0.17413E-01 0.38701E-01
   Dimensionless distance   yplus :  0.42719E+03 0.95246E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60733E+01      61   0.12566E-02   0.19898E-01 
c  VelocityX    0.46299E+04      12   0.64269E-02   0.40236E-03 
c  VelocityY    0.46299E+04      12   0.64269E-02   0.27190E-04 
c  VelocityZ    0.46299E+04      12   0.64269E-02   0.51510E-04 
c  TurbEner     0.59747E+01      14   0.13002E-03   0.20661E-08 
c  Dissip       0.14724E+01      16   0.21967E-02   0.72132E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.97           54509           26776           27270
v  Velocity[x]            0.29276          2.0925         0.90806         0.90984
v  Velocity[y]            -0.3825          0.6949      0.00055717      0.00033649
v  Velocity[z]           -0.42087         0.51115      -0.0012383      -0.0013575
v  TurbEner             0.0010129        0.014942       0.0032845       0.0033442
v  Dissip              9.2111e-05         0.03099      0.00045163      0.00039041
v  TurbVisc               0.16448          11.338          4.7118          5.2731
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              428:        0.96377E-01

===============================================================


 INSTANT    0.429000000E+03   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001192E+04
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 :  0.23785E+00 0.12136E+01
   Friction velocity        uet   :  0.14228E-01 0.72341E-01
   Friction velocity        uk    :  0.17432E-01 0.38776E-01
   Dimensionless distance   yplus :  0.42811E+03 0.95242E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60317E+01      54   0.12654E-02   0.19777E-01 
c  VelocityX    0.46299E+04      13   0.61851E-02   0.29702E-03 
c  VelocityY    0.46299E+04      13   0.61851E-02   0.26345E-04 
c  VelocityZ    0.46299E+04      13   0.61851E-02   0.52029E-04 
c  TurbEner     0.59751E+01      12   0.64074E-04   0.62662E-09 
c  Dissip       0.14751E+01      14   0.51444E-03   0.36338E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.83           54526           26776           27270
v  Velocity[x]            0.29246          2.1418         0.90805         0.90983
v  Velocity[y]           -0.36817         0.70271      0.00054664       0.0003234
v  Velocity[z]           -0.42151         0.50408      -0.0012522      -0.0013728
v  TurbEner             0.0010111        0.014837       0.0032845       0.0033442
v  Dissip              9.2166e-05        0.030678      0.00045157      0.00039036
v  TurbVisc               0.16498          11.326          4.7118          5.2731
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              429:        0.95738E-01

===============================================================


 INSTANT    0.430000000E+03   TIME STEP NUMBER             430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001010E+04
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 :  0.23778E+00 0.13250E+01
   Friction velocity        uet   :  0.14222E-01 0.78982E-01
   Friction velocity        uk    :  0.17416E-01 0.38788E-01
   Dimensionless distance   yplus :  0.42805E+03 0.95251E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61550E+01      58   0.13036E-02   0.20180E-01 
c  VelocityX    0.46298E+04      12   0.69015E-02   0.34816E-03 
c  VelocityY    0.46298E+04      12   0.69015E-02   0.55712E-04 
c  VelocityZ    0.46298E+04      12   0.69015E-02   0.10011E-03 
c  TurbEner     0.59763E+01      12   0.66831E-04   0.70780E-09 
c  Dissip       0.14975E+01      15   0.70401E-03   0.11797E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.87           54539           26776           27271
v  Velocity[x]            0.29276          2.1838         0.90805         0.90983
v  Velocity[y]           -0.38302         0.69234      0.00055886      0.00033565
v  Velocity[z]           -0.42045         0.51142      -0.0012376      -0.0013584
v  TurbEner             0.0010133        0.014934       0.0032846       0.0033443
v  Dissip              9.2175e-05        0.030909      0.00045168      0.00039042
v  TurbVisc               0.16484          11.363          4.7118          5.2732
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              430:        0.96192E-01

===============================================================


 INSTANT    0.431000000E+03   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997760E+04
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 :  0.23750E+00 0.12174E+01
   Friction velocity        uet   :  0.14204E-01 0.72570E-01
   Friction velocity        uk    :  0.17435E-01 0.38756E-01
   Dimensionless distance   yplus :  0.42763E+03 0.95194E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54390E+01      59   0.13085E-02   0.17840E-01 
c  VelocityX    0.46298E+04      12   0.66418E-02   0.33532E-03 
c  VelocityY    0.46298E+04      12   0.66418E-02   0.25883E-04 
c  VelocityZ    0.46298E+04      12   0.66418E-02   0.45815E-04 
c  TurbEner     0.59768E+01      13   0.12035E-03   0.12978E-08 
c  Dissip       0.15116E+01      16   0.20470E-02   0.47834E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.94           54549           26777           27271
v  Velocity[x]            0.29308          2.0162         0.90803         0.90981
v  Velocity[y]           -0.36802         0.70027      0.00055442      0.00032832
v  Velocity[z]           -0.42051         0.50706      -0.0012518      -0.0013708
v  TurbEner             0.0010162        0.015515       0.0032848       0.0033444
v  Dissip              9.2128e-05        0.032499      0.00045189      0.00039058
v  TurbVisc               0.16464          11.346          4.7119          5.2732
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              431:        0.96195E-01

===============================================================


 INSTANT    0.432000000E+03   TIME STEP NUMBER             432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998101E+04
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 :  0.23779E+00 0.13242E+01
   Friction velocity        uet   :  0.14221E-01 0.78931E-01
   Friction velocity        uk    :  0.17461E-01 0.38708E-01
   Dimensionless distance   yplus :  0.42884E+03 0.95183E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60582E+01      57   0.15496E-02   0.19870E-01 
c  VelocityX    0.46299E+04      12   0.73193E-02   0.33390E-03 
c  VelocityY    0.46299E+04      12   0.73193E-02   0.23997E-04 
c  VelocityZ    0.46299E+04      12   0.73193E-02   0.50148E-04 
c  TurbEner     0.59757E+01      14   0.13587E-03   0.19955E-08 
c  Dissip       0.14790E+01      16   0.21217E-02   0.69105E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.58           54543           26778           27272
v  Velocity[x]            0.29252          2.0918         0.90805         0.90983
v  Velocity[y]           -0.38291         0.69559      0.00054522      0.00032556
v  Velocity[z]           -0.42022         0.51382      -0.0012417      -0.0013657
v  TurbEner             0.0010127        0.014914       0.0032847       0.0033443
v  Dissip              9.2094e-05        0.031177      0.00045169      0.00039045
v  TurbVisc               0.16528          11.348           4.712          5.2733
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              432:        0.96272E-01

===============================================================


 INSTANT    0.433000000E+03   TIME STEP NUMBER             433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997765E+04
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 :  0.23767E+00 0.12137E+01
   Friction velocity        uet   :  0.14215E-01 0.72356E-01
   Friction velocity        uk    :  0.17430E-01 0.38667E-01
   Dimensionless distance   yplus :  0.42846E+03 0.95107E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65445E+01      56   0.16151E-02   0.21452E-01 
c  VelocityX    0.46299E+04      13   0.69017E-02   0.44156E-03 
c  VelocityY    0.46299E+04      13   0.69017E-02   0.28026E-04 
c  VelocityZ    0.46299E+04      13   0.69017E-02   0.55254E-04 
c  TurbEner     0.59758E+01      13   0.77786E-04   0.11646E-08 
c  Dissip       0.14828E+01      14   0.53982E-03   0.45075E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.45           54518           26778           27272
v  Velocity[x]            0.29272          2.1399         0.90806         0.90984
v  Velocity[y]           -0.36662         0.70428      0.00055329      0.00033137
v  Velocity[z]           -0.42011         0.50788      -0.0012444      -0.0013626
v  TurbEner             0.0010153        0.014762       0.0032846       0.0033444
v  Dissip              9.2049e-05        0.030852      0.00045163      0.00039042
v  TurbVisc               0.16496          11.323           4.712          5.2733
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              433:        0.96163E-01

===============================================================


 INSTANT    0.434000000E+03   TIME STEP NUMBER             434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998658E+04
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 :  0.23786E+00 0.13249E+01
   Friction velocity        uet   :  0.14227E-01 0.78980E-01
   Friction velocity        uk    :  0.17452E-01 0.38734E-01
   Dimensionless distance   yplus :  0.42825E+03 0.95103E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.79110E+01      61   0.15044E-02   0.25927E-01 
c  VelocityX    0.46299E+04      13   0.71066E-02   0.39634E-03 
c  VelocityY    0.46299E+04      13   0.71066E-02   0.61936E-04 
c  VelocityZ    0.46299E+04      13   0.71066E-02   0.10360E-03 
c  TurbEner     0.59762E+01      12   0.74153E-04   0.10178E-08 
c  Dissip       0.15042E+01      15   0.70223E-03   0.12494E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.64           54534           26778           27272
v  Velocity[x]            0.29275          2.1871         0.90803         0.90981
v  Velocity[y]           -0.38268         0.69234      0.00056491      0.00034309
v  Velocity[z]           -0.42104         0.51206      -0.0012342      -0.0013566
v  TurbEner             0.0010151        0.014805       0.0032848       0.0033445
v  Dissip               9.201e-05        0.030963      0.00045176       0.0003905
v  TurbVisc               0.16486          11.318           4.712          5.2733
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              434:        0.96805E-01

===============================================================


 INSTANT    0.435000000E+03   TIME STEP NUMBER             435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000311E+04
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 :  0.23785E+00 0.12182E+01
   Friction velocity        uet   :  0.14226E-01 0.72611E-01
   Friction velocity        uk    :  0.17451E-01 0.38761E-01
   Dimensionless distance   yplus :  0.42867E+03 0.95100E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71896E+01      64   0.14473E-02   0.23587E-01 
c  VelocityX    0.46299E+04      12   0.66537E-02   0.40697E-03 
c  VelocityY    0.46299E+04      12   0.66537E-02   0.65506E-04 
c  VelocityZ    0.46299E+04      12   0.66537E-02   0.57980E-04 
c  TurbEner     0.59763E+01      14   0.13847E-03   0.18535E-08 
c  Dissip       0.15098E+01      16   0.19734E-02   0.41827E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.21           54524           26778           27272
v  Velocity[x]            0.29285          2.0048         0.90804         0.90982
v  Velocity[y]           -0.36807         0.70112      0.00055587      0.00033075
v  Velocity[z]           -0.42218         0.50503      -0.0012538      -0.0013748
v  TurbEner             0.0010121        0.015459       0.0032847       0.0033444
v  Dissip              9.2033e-05        0.032498      0.00045189      0.00039061
v  TurbVisc                0.1651          11.345          4.7121          5.2734
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              435:        0.98070E-01

===============================================================


 INSTANT    0.436000000E+03   TIME STEP NUMBER             436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000010E+04
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 :  0.23747E+00 0.13243E+01
   Friction velocity        uet   :  0.14204E-01 0.78936E-01
   Friction velocity        uk    :  0.17425E-01 0.38722E-01
   Dimensionless distance   yplus :  0.42849E+03 0.95085E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66688E+01      60   0.14562E-02   0.21860E-01 
c  VelocityX    0.46298E+04      12   0.70074E-02   0.35074E-03 
c  VelocityY    0.46298E+04      12   0.70074E-02   0.35990E-04 
c  VelocityZ    0.46298E+04      12   0.70074E-02   0.33388E-04 
c  TurbEner     0.59754E+01      13   0.14357E-03   0.19517E-08 
c  Dissip       0.14759E+01      16   0.23729E-02   0.73242E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.75           54506           26778           27273
v  Velocity[x]             0.2929          2.1019         0.90804         0.90982
v  Velocity[y]           -0.38264         0.69532      0.00055507      0.00033405
v  Velocity[z]           -0.41957         0.51226       -0.001244      -0.0013654
v  TurbEner             0.0010126        0.014778       0.0032846       0.0033444
v  Dissip              9.2055e-05        0.030876      0.00045165      0.00039044
v  TurbVisc                0.1649          11.328          4.7121          5.2734
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              436:        0.97165E-01

===============================================================


 INSTANT    0.437000000E+03   TIME STEP NUMBER             437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998958E+04
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 :  0.23746E+00 0.12176E+01
   Friction velocity        uet   :  0.14205E-01 0.72587E-01
   Friction velocity        uk    :  0.17429E-01 0.38704E-01
   Dimensionless distance   yplus :  0.42781E+03 0.95141E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64536E+01      55   0.12148E-02   0.21156E-01 
c  VelocityX    0.46299E+04      12   0.73507E-02   0.34599E-03 
c  VelocityY    0.46299E+04      12   0.73507E-02   0.34309E-04 
c  VelocityZ    0.46299E+04      12   0.73507E-02   0.44952E-04 
c  TurbEner     0.59752E+01      13   0.66629E-04   0.11421E-08 
c  Dissip       0.14776E+01      14   0.32640E-03   0.24674E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.22           54518           26778           27272
v  Velocity[x]             0.2928          2.1389         0.90806         0.90984
v  Velocity[y]           -0.36671         0.70202      0.00054655      0.00032247
v  Velocity[z]           -0.41958         0.50637      -0.0012529      -0.0013705
v  TurbEner             0.0010137        0.014741       0.0032847       0.0033444
v  Dissip              9.2057e-05          0.0307      0.00045161      0.00039041
v  TurbVisc               0.16463          11.335          4.7121          5.2734
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              437:        0.95449E-01

===============================================================


 INSTANT    0.438000000E+03   TIME STEP NUMBER             438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002089E+04
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 :  0.23772E+00 0.13267E+01
   Friction velocity        uet   :  0.14221E-01 0.79085E-01
   Friction velocity        uk    :  0.17439E-01 0.38721E-01
   Dimensionless distance   yplus :  0.42864E+03 0.95195E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73363E+01      59   0.15239E-02   0.24044E-01 
c  VelocityX    0.46300E+04      13   0.72420E-02   0.39362E-03 
c  VelocityY    0.46300E+04      13   0.72420E-02   0.40188E-04 
c  VelocityZ    0.46300E+04      13   0.72420E-02   0.75127E-04 
c  TurbEner     0.59766E+01      13   0.77309E-04   0.10741E-08 
c  Dissip       0.15011E+01      15   0.71634E-03   0.12236E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.28           54532           26777           27271
v  Velocity[x]            0.29253          2.1845         0.90804         0.90982
v  Velocity[y]           -0.38237         0.69558       0.0005441      0.00032023
v  Velocity[z]           -0.41933         0.51131      -0.0012409      -0.0013649
v  TurbEner             0.0010088        0.014844       0.0032848       0.0033445
v  Dissip              9.2101e-05        0.030926      0.00045174      0.00039049
v  TurbVisc               0.16513          11.374          4.7122          5.2735
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              438:        0.96660E-01

===============================================================


 INSTANT    0.439000000E+03   TIME STEP NUMBER             439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001414E+04
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 :  0.23766E+00 0.12141E+01
   Friction velocity        uet   :  0.14218E-01 0.72371E-01
   Friction velocity        uk    :  0.17397E-01 0.38670E-01
   Dimensionless distance   yplus :  0.42796E+03 0.95206E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66439E+01      58   0.13698E-02   0.21782E-01 
c  VelocityX    0.46299E+04      13   0.65637E-02   0.42965E-03 
c  VelocityY    0.46299E+04      13   0.65637E-02   0.33642E-04 
c  VelocityZ    0.46299E+04      13   0.65637E-02   0.61908E-04 
c  TurbEner     0.59766E+01      13   0.13091E-03   0.14267E-08 
c  Dissip       0.15070E+01      16   0.19124E-02   0.38995E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.83           54542           26777           27271
v  Velocity[x]            0.29288          2.0072         0.90806         0.90984
v  Velocity[y]           -0.36701         0.70393      0.00054972      0.00032358
v  Velocity[z]           -0.41903         0.50487      -0.0012589      -0.0013798
v  TurbEner             0.0010105        0.015474       0.0032849       0.0033445
v  Dissip              9.2116e-05        0.032419      0.00045192      0.00039062
v  TurbVisc               0.16468          11.356          4.7123          5.2736
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              439:        0.96505E-01

===============================================================


 INSTANT    0.440000000E+03   TIME STEP NUMBER             440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001257E+04
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 :  0.23765E+00 0.13253E+01
   Friction velocity        uet   :  0.14218E-01 0.79003E-01
   Friction velocity        uk    :  0.17411E-01 0.38677E-01
   Dimensionless distance   yplus :  0.42749E+03 0.95271E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56921E+01      55   0.12583E-02   0.18659E-01 
c  VelocityX    0.46299E+04      13   0.62890E-02   0.32111E-03 
c  VelocityY    0.46299E+04      13   0.62890E-02   0.23023E-04 
c  VelocityZ    0.46299E+04      13   0.62890E-02   0.34260E-04 
c  TurbEner     0.59757E+01      14   0.15827E-03   0.21868E-08 
c  Dissip       0.14622E+01      17   0.27216E-02   0.93891E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.48           54549           26777           27271
v  Velocity[x]            0.29304          2.0983         0.90805         0.90982
v  Velocity[y]           -0.38245         0.69126      0.00054026      0.00031805
v  Velocity[z]           -0.42144          0.5119      -0.0012571      -0.0013784
v  TurbEner             0.0010103        0.014707        0.003285       0.0033446
v  Dissip              9.2095e-05        0.030554      0.00045166      0.00039044
v  TurbVisc                0.1646          11.357          4.7122          5.2735
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              440:        0.95340E-01

===============================================================


 INSTANT    0.441000000E+03   TIME STEP NUMBER             441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999098E+04
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 :  0.23752E+00 0.12181E+01
   Friction velocity        uet   :  0.14210E-01 0.72606E-01
   Friction velocity        uk    :  0.17409E-01 0.38676E-01
   Dimensionless distance   yplus :  0.42786E+03 0.95285E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66112E+01      54   0.14801E-02   0.21672E-01 
c  VelocityX    0.46299E+04      12   0.74200E-02   0.31247E-03 
c  VelocityY    0.46299E+04      12   0.74200E-02   0.36958E-04 
c  VelocityZ    0.46299E+04      12   0.74200E-02   0.36627E-04 
c  TurbEner     0.59765E+01      13   0.69319E-04   0.79938E-09 
c  Dissip       0.14628E+01      14   0.45809E-03   0.31414E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.97           54542           26777           27271
v  Velocity[x]            0.29263          2.1368         0.90806         0.90984
v  Velocity[y]           -0.36692         0.70008      0.00054515      0.00032645
v  Velocity[z]           -0.41925         0.50581      -0.0012588      -0.0013777
v  TurbEner             0.0010074        0.014655       0.0032852       0.0033448
v  Dissip              9.2075e-05        0.030264       0.0004516       0.0003904
v  TurbVisc                0.1649          11.333          4.7124          5.2737
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              441:        0.95162E-01

===============================================================


 INSTANT    0.442000000E+03   TIME STEP NUMBER             442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001860E+04
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 :  0.23747E+00 0.13234E+01
   Friction velocity        uet   :  0.14207E-01 0.78884E-01
   Friction velocity        uk    :  0.17385E-01 0.38733E-01
   Dimensionless distance   yplus :  0.42761E+03 0.95245E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64342E+01      63   0.15662E-02   0.21092E-01 
c  VelocityX    0.46300E+04      12   0.73200E-02   0.41309E-03 
c  VelocityY    0.46300E+04      12   0.73200E-02   0.24525E-04 
c  VelocityZ    0.46300E+04      12   0.73200E-02   0.81752E-04 
c  TurbEner     0.59777E+01      13   0.79328E-04   0.13521E-08 
c  Dissip       0.14847E+01      15   0.81366E-03   0.14450E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.06           54522           26778           27272
v  Velocity[x]            0.29263          2.1773         0.90806         0.90984
v  Velocity[y]           -0.38285         0.69416      0.00055195      0.00033325
v  Velocity[z]           -0.41834         0.51051      -0.0012364      -0.0013576
v  TurbEner             0.0010087        0.014848       0.0032853        0.003345
v  Dissip              9.2108e-05        0.030645      0.00045172      0.00039049
v  TurbVisc               0.16477          11.324          4.7125          5.2737
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              442:        0.96403E-01

===============================================================


 INSTANT    0.443000000E+03   TIME STEP NUMBER             443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997998E+04
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 :  0.23756E+00 0.12162E+01
   Friction velocity        uet   :  0.14213E-01 0.72501E-01
   Friction velocity        uk    :  0.17396E-01 0.38744E-01
   Dimensionless distance   yplus :  0.42696E+03 0.95233E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63201E+01      56   0.13418E-02   0.20715E-01 
c  VelocityX    0.46300E+04      13   0.65981E-02   0.41117E-03 
c  VelocityY    0.46300E+04      13   0.65981E-02   0.33922E-04 
c  VelocityZ    0.46300E+04      13   0.65981E-02   0.49115E-04 
c  TurbEner     0.59780E+01      13   0.88276E-04   0.12079E-08 
c  Dissip       0.15090E+01      15   0.98474E-03   0.18424E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.12           54528           26778           27272
v  Velocity[x]              0.293          2.1971         0.90806         0.90984
v  Velocity[y]           -0.36732         0.70335      0.00054755      0.00032436
v  Velocity[z]           -0.41977         0.50444      -0.0012515      -0.0013692
v  TurbEner             0.0010108        0.015075       0.0032854        0.003345
v  Dissip              9.2111e-05        0.031221      0.00045191      0.00039063
v  TurbVisc               0.16453          11.357          4.7124          5.2737
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              443:        0.96166E-01

===============================================================


 INSTANT    0.444000000E+03   TIME STEP NUMBER             444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997799E+04
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 :  0.23761E+00 0.13247E+01
   Friction velocity        uet   :  0.14216E-01 0.78963E-01
   Friction velocity        uk    :  0.17414E-01 0.38771E-01
   Dimensionless distance   yplus :  0.42784E+03 0.95227E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62395E+01      55   0.14612E-02   0.20462E-01 
c  VelocityX    0.46300E+04      12   0.63785E-02   0.33873E-03 
c  VelocityY    0.46300E+04      12   0.63785E-02   0.27189E-04 
c  VelocityZ    0.46300E+04      12   0.63785E-02   0.25288E-04 
c  TurbEner     0.59786E+01      13   0.12569E-03   0.14867E-08 
c  Dissip       0.15294E+01      16   0.22065E-02   0.54638E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.55           54537           26778           27272
v  Velocity[x]            0.29242           2.035         0.90805         0.90982
v  Velocity[y]           -0.38216         0.69522      0.00054459      0.00032629
v  Velocity[z]           -0.41905         0.51197      -0.0012541      -0.0013759
v  TurbEner             0.0010075        0.015671       0.0032855       0.0033451
v  Dissip                9.21e-05        0.032975      0.00045217      0.00039082
v  TurbVisc               0.16508          11.405          4.7124          5.2737
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              444:        0.95491E-01

===============================================================


 INSTANT    0.445000000E+03   TIME STEP NUMBER             445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998631E+04
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 :  0.23811E+00 0.12174E+01
   Friction velocity        uet   :  0.14246E-01 0.72573E-01
   Friction velocity        uk    :  0.17385E-01 0.38697E-01
   Dimensionless distance   yplus :  0.42744E+03 0.95210E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63223E+01      54   0.14095E-02   0.20734E-01 
c  VelocityX    0.46298E+04      12   0.65883E-02   0.46118E-03 
c  VelocityY    0.46298E+04      12   0.65883E-02   0.39409E-04 
c  VelocityZ    0.46298E+04      12   0.65883E-02   0.47514E-04 
c  TurbEner     0.59767E+01      13   0.10694E-03   0.14433E-08 
c  Dissip       0.14852E+01      16   0.14693E-02   0.52873E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.96           54544           26778           27272
v  Velocity[x]            0.29274          1.7199         0.90803         0.90981
v  Velocity[y]           -0.36604         0.70086      0.00053802      0.00031723
v  Velocity[z]           -0.41963         0.50658      -0.0012651      -0.0013846
v  TurbEner             0.0010106        0.015537       0.0032854       0.0033451
v  Dissip              9.2087e-05        0.032861      0.00045196      0.00039071
v  TurbVisc                0.1648          11.393          4.7124          5.2737
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              445:        0.95731E-01

===============================================================


 INSTANT    0.446000000E+03   TIME STEP NUMBER             446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001795E+04
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 :  0.23750E+00 0.13254E+01
   Friction velocity        uet   :  0.14209E-01 0.78997E-01
   Friction velocity        uk    :  0.17412E-01 0.38721E-01
   Dimensionless distance   yplus :  0.42734E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56353E+01      51   0.12129E-02   0.18482E-01 
c  VelocityX    0.46297E+04      13   0.61992E-02   0.33498E-03 
c  VelocityY    0.46297E+04      13   0.61992E-02   0.25552E-04 
c  VelocityZ    0.46297E+04      13   0.61992E-02   0.64114E-04 
c  TurbEner     0.59724E+01      15   0.39107E-03   0.81597E-08 
c  Dissip       0.13440E+01      18   0.78566E-02   0.44229E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.76           54552           26778           27272
v  Velocity[x]              0.293          1.8806         0.90803         0.90981
v  Velocity[y]           -0.38225         0.69437      0.00053907      0.00031999
v  Velocity[z]           -0.41987         0.51116      -0.0012478       -0.001369
v  TurbEner             0.0010117        0.013413       0.0032852       0.0033449
v  Dissip              9.2103e-05        0.027409      0.00045135      0.00039025
v  TurbVisc               0.16477           11.34          4.7124          5.2736
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              446:        0.96570E-01

===============================================================


 INSTANT    0.447000000E+03   TIME STEP NUMBER             447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998894E+04
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 :  0.23759E+00 0.12134E+01
   Friction velocity        uet   :  0.14215E-01 0.72283E-01
   Friction velocity        uk    :  0.17421E-01 0.38756E-01
   Dimensionless distance   yplus :  0.42801E+03 0.95208E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59795E+01      57   0.15656E-02   0.19604E-01 
c  VelocityX    0.46299E+04      13   0.74301E-02   0.33858E-03 
c  VelocityY    0.46299E+04      13   0.74301E-02   0.25734E-04 
c  VelocityZ    0.46299E+04      13   0.74301E-02   0.36579E-04 
c  TurbEner     0.59710E+01      14   0.15475E-03   0.21871E-08 
c  Dissip       0.12874E+01      18   0.37055E-02   0.12931E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.68           54543           26778           27272
v  Velocity[x]            0.29251          1.9892         0.90806         0.90983
v  Velocity[y]            -0.3677         0.70294        0.000547      0.00032613
v  Velocity[z]           -0.41996         0.50423      -0.0012542      -0.0013768
v  TurbEner             0.0010095        0.012709       0.0032848       0.0033447
v  Dissip              9.2101e-05        0.025072       0.0004507       0.0003898
v  TurbVisc               0.16512          11.329          4.7124          5.2737
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              447:        0.96930E-01

===============================================================


 INSTANT    0.448000000E+03   TIME STEP NUMBER             448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001879E+04
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 :  0.23782E+00 0.13249E+01
   Friction velocity        uet   :  0.14228E-01 0.78974E-01
   Friction velocity        uk    :  0.17402E-01 0.38775E-01
   Dimensionless distance   yplus :  0.42792E+03 0.95173E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67206E+01      56   0.15880E-02   0.22034E-01 
c  VelocityX    0.46299E+04      12   0.68445E-02   0.49556E-03 
c  VelocityY    0.46299E+04      12   0.68445E-02   0.24795E-04 
c  VelocityZ    0.46299E+04      12   0.68445E-02   0.51816E-04 
c  TurbEner     0.59706E+01      13   0.93778E-04   0.16511E-08 
c  Dissip       0.12525E+01      18   0.23758E-02   0.87856E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.91           54518           26777           27272
v  Velocity[x]            0.29257          2.0673         0.90806         0.90984
v  Velocity[y]           -0.38241          0.6926      0.00055094      0.00033109
v  Velocity[z]            -0.4197         0.51179      -0.0012417      -0.0013612
v  TurbEner             0.0010112         0.01263       0.0032846       0.0033445
v  Dissip              9.2105e-05        0.024118      0.00045007      0.00038938
v  TurbVisc               0.16491           11.35          4.7124          5.2736
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              448:        0.96060E-01

===============================================================


 INSTANT    0.449000000E+03   TIME STEP NUMBER             449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001967E+04
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 :  0.23755E+00 0.12176E+01
   Friction velocity        uet   :  0.14212E-01 0.72577E-01
   Friction velocity        uk    :  0.17417E-01 0.38783E-01
   Dimensionless distance   yplus :  0.42741E+03 0.95146E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57300E+01      57   0.11987E-02   0.18781E-01 
c  VelocityX    0.46299E+04      12   0.70515E-02   0.34925E-03 
c  VelocityY    0.46299E+04      12   0.70515E-02   0.34726E-04 
c  VelocityZ    0.46299E+04      12   0.70515E-02   0.55640E-04 
c  TurbEner     0.59704E+01      13   0.77946E-04   0.13458E-08 
c  Dissip       0.12405E+01      17   0.10691E-02   0.22687E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.13           54523           26776           27270
v  Velocity[x]            0.29337            2.12         0.90804         0.90982
v  Velocity[y]           -0.36611         0.70006      0.00055228      0.00032967
v  Velocity[z]            -0.4179         0.50644      -0.0012534      -0.0013721
v  TurbEner             0.0010137        0.012822       0.0032845       0.0033444
v  Dissip              9.2076e-05        0.023787      0.00044951      0.00038899
v  TurbVisc               0.16468          11.331          4.7125          5.2737
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              449:        0.96610E-01

===============================================================


 INSTANT    0.450000000E+03   TIME STEP NUMBER             450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002045E+04
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 :  0.23758E+00 0.13240E+01
   Friction velocity        uet   :  0.14214E-01 0.78913E-01
   Friction velocity        uk    :  0.17439E-01 0.38774E-01
   Dimensionless distance   yplus :  0.42844E+03 0.95108E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61432E+01      52   0.12775E-02   0.20150E-01 
c  VelocityX    0.46299E+04      13   0.70267E-02   0.32883E-03 
c  VelocityY    0.46299E+04      13   0.70267E-02   0.42219E-04 
c  VelocityZ    0.46299E+04      13   0.70267E-02   0.98535E-04 
c  TurbEner     0.59716E+01      13   0.97296E-04   0.11888E-08 
c  Dissip       0.12464E+01      16   0.62371E-03   0.70900E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.77           54532           26776           27271
v  Velocity[x]            0.29266          2.1537         0.90805         0.90983
v  Velocity[y]           -0.38238         0.69516      0.00054856      0.00032712
v  Velocity[z]           -0.41925         0.51087      -0.0012473      -0.0013686
v  TurbEner             0.0010103        0.013292       0.0032845       0.0033445
v  Dissip              9.2096e-05        0.024132      0.00044919      0.00038876
v  TurbVisc               0.16524          11.336          4.7126          5.2738
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              450:        0.96167E-01

===============================================================


 INSTANT    0.451000000E+03   TIME STEP NUMBER             451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999557E+04
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 :  0.23791E+00 0.12231E+01
   Friction velocity        uet   :  0.14233E-01 0.72316E-01
   Friction velocity        uk    :  0.17410E-01 0.38675E-01
   Dimensionless distance   yplus :  0.42803E+03 0.95176E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56682E+01      54   0.12393E-02   0.18579E-01 
c  VelocityX    0.46300E+04      13   0.75107E-02   0.33959E-03 
c  VelocityY    0.46300E+04      13   0.75107E-02   0.24316E-04 
c  VelocityZ    0.46300E+04      13   0.75107E-02   0.53482E-04 
c  TurbEner     0.59732E+01      13   0.11077E-03   0.16193E-08 
c  Dissip       0.12677E+01      16   0.10220E-02   0.15054E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.89           54542           26776           27271
v  Velocity[x]            0.29253          2.1828         0.90806         0.90984
v  Velocity[y]           -0.36795         0.70428      0.00054701      0.00032077
v  Velocity[z]           -0.42122         0.50401      -0.0012586      -0.0013785
v  TurbEner             0.0010132        0.013793       0.0032846       0.0033445
v  Dissip              9.2059e-05          0.0248      0.00044905      0.00038866
v  TurbVisc               0.16491          11.375          4.7128           5.274
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              451:        0.96249E-01

===============================================================


 INSTANT    0.452000000E+03   TIME STEP NUMBER             452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999498E+04
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 :  0.23768E+00 0.13250E+01
   Friction velocity        uet   :  0.14219E-01 0.78980E-01
   Friction velocity        uk    :  0.17434E-01 0.38687E-01
   Dimensionless distance   yplus :  0.42783E+03 0.95172E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60941E+01      55   0.15135E-02   0.19981E-01 
c  VelocityX    0.46299E+04      13   0.66647E-02   0.33547E-03 
c  VelocityY    0.46299E+04      13   0.66647E-02   0.24382E-04 
c  VelocityZ    0.46299E+04      13   0.66647E-02   0.33277E-04 
c  TurbEner     0.59746E+01      14   0.15818E-03   0.24452E-08 
c  Dissip       0.12893E+01      17   0.23223E-02   0.56826E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.67           54550           26777           27271
v  Velocity[x]            0.29296           2.022         0.90805         0.90983
v  Velocity[y]           -0.38301         0.69206      0.00055085      0.00032779
v  Velocity[z]           -0.42038         0.51121      -0.0012556       -0.001375
v  TurbEner             0.0010134        0.014656        0.003285       0.0033448
v  Dissip              9.2089e-05        0.026564      0.00044912      0.00038872
v  TurbVisc               0.16484          11.343           4.713          5.2742
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              452:        0.95419E-01

===============================================================


 INSTANT    0.453000000E+03   TIME STEP NUMBER             453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998808E+04
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 :  0.23800E+00 0.12178E+01
   Friction velocity        uet   :  0.14237E-01 0.72582E-01
   Friction velocity        uk    :  0.17436E-01 0.38738E-01
   Dimensionless distance   yplus :  0.42824E+03 0.95172E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63726E+01      67   0.14771E-02   0.20897E-01 
c  VelocityX    0.46300E+04      12   0.73038E-02   0.32990E-03 
c  VelocityY    0.46300E+04      12   0.73038E-02   0.38303E-04 
c  VelocityZ    0.46300E+04      12   0.73038E-02   0.35509E-04 
c  TurbEner     0.59748E+01      13   0.95338E-04   0.12656E-08 
c  Dissip       0.12780E+01      16   0.12132E-02   0.20634E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.37           54543           26778           27272
v  Velocity[x]            0.29281          2.0888         0.90807         0.90985
v  Velocity[y]           -0.36816         0.70071      0.00054687      0.00032542
v  Velocity[z]           -0.42084         0.50692      -0.0012571      -0.0013778
v  TurbEner             0.0010111        0.014301       0.0032851        0.003345
v  Dissip              9.2115e-05        0.025774      0.00044893       0.0003886
v  TurbVisc               0.16509          11.339          4.7133          5.2744
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              453:        0.98933E-01

===============================================================


 INSTANT    0.454000000E+03   TIME STEP NUMBER             454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998904E+04
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 :  0.23790E+00 0.13240E+01
   Friction velocity        uet   :  0.14231E-01 0.78920E-01
   Friction velocity        uk    :  0.17416E-01 0.38771E-01
   Dimensionless distance   yplus :  0.42815E+03 0.95198E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64843E+01      55   0.14954E-02   0.21259E-01 
c  VelocityX    0.46301E+04      12   0.70412E-02   0.44446E-03 
c  VelocityY    0.46301E+04      12   0.70412E-02   0.24987E-04 
c  VelocityZ    0.46301E+04      12   0.70412E-02   0.33785E-04 
c  TurbEner     0.59760E+01      13   0.70251E-04   0.11944E-08 
c  Dissip       0.12967E+01      15   0.56263E-03   0.74963E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.94           54518           26778           27272
v  Velocity[x]            0.29252           2.147         0.90808         0.90986
v  Velocity[y]           -0.38284         0.69474      0.00055385      0.00033635
v  Velocity[z]           -0.42172         0.51378      -0.0012436      -0.0013638
v  TurbEner             0.0010123        0.014394       0.0032854       0.0033452
v  Dissip              9.2133e-05        0.026032      0.00044901      0.00038868
v  TurbVisc               0.16497          11.367          4.7135          5.2747
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              454:        0.95872E-01

===============================================================


 INSTANT    0.455000000E+03   TIME STEP NUMBER             455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998381E+04
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 :  0.23735E+00 0.12170E+01
   Friction velocity        uet   :  0.14198E-01 0.72548E-01
   Friction velocity        uk    :  0.17427E-01 0.38752E-01
   Dimensionless distance   yplus :  0.42757E+03 0.95169E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58548E+01      52   0.12196E-02   0.19193E-01 
c  VelocityX    0.46302E+04      12   0.75054E-02   0.37477E-03 
c  VelocityY    0.46302E+04      12   0.75054E-02   0.25430E-04 
c  VelocityZ    0.46302E+04      12   0.75054E-02   0.40213E-04 
c  TurbEner     0.59769E+01      13   0.90635E-04   0.16196E-08 
c  Dissip       0.13266E+01      16   0.12477E-02   0.31693E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.65           54523           26778           27272
v  Velocity[x]            0.29305          2.1759         0.90805         0.90984
v  Velocity[y]           -0.36651          0.7031      0.00054753      0.00032392
v  Velocity[z]           -0.41871         0.50792      -0.0012539      -0.0013731
v  TurbEner             0.0010143        0.014655       0.0032857       0.0033455
v  Dissip              9.2177e-05        0.026699      0.00044925      0.00038884
v  TurbVisc               0.16474          11.344          4.7138          5.2749
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              455:        0.95666E-01

===============================================================


 INSTANT    0.456000000E+03   TIME STEP NUMBER             456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000491E+04
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 :  0.23762E+00 0.13242E+01
   Friction velocity        uet   :  0.14213E-01 0.78934E-01
   Friction velocity        uk    :  0.17444E-01 0.38714E-01
   Dimensionless distance   yplus :  0.42855E+03 0.95197E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65102E+01      54   0.13188E-02   0.21352E-01 
c  VelocityX    0.46301E+04      12   0.68570E-02   0.43343E-03 
c  VelocityY    0.46301E+04      12   0.68570E-02   0.33809E-04 
c  VelocityZ    0.46301E+04      12   0.68570E-02   0.13013E-03 
c  TurbEner     0.59778E+01      14   0.13292E-03   0.18340E-08 
c  Dissip       0.13524E+01      17   0.22830E-02   0.62962E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.8           54527           26778           27273
v  Velocity[x]            0.29257          2.0155         0.90805         0.90984
v  Velocity[y]           -0.38268         0.69566      0.00055569      0.00033658
v  Velocity[z]           -0.42067         0.51214      -0.0012473      -0.0013681
v  TurbEner             0.0010102        0.015366        0.003286       0.0033456
v  Dissip              9.2185e-05         0.02848      0.00044958      0.00038908
v  TurbVisc               0.16533          11.337           4.714          5.2751
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              456:        0.95788E-01

===============================================================


 INSTANT    0.457000000E+03   TIME STEP NUMBER             457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999606E+04
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 :  0.23781E+00 0.12241E+01
   Friction velocity        uet   :  0.14224E-01 0.72549E-01
   Friction velocity        uk    :  0.17409E-01 0.38493E-01
   Dimensionless distance   yplus :  0.42803E+03 0.95272E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55952E+01      61   0.13416E-02   0.18363E-01 
c  VelocityX    0.46301E+04      12   0.65620E-02   0.33776E-03 
c  VelocityY    0.46301E+04      12   0.65620E-02   0.27189E-04 
c  VelocityZ    0.46301E+04      12   0.65620E-02   0.44132E-04 
c  TurbEner     0.59770E+01      13   0.11101E-03   0.16019E-08 
c  Dissip       0.13387E+01      16   0.13501E-02   0.27573E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.96           54507           26778           27273
v  Velocity[x]             0.2928          2.0935         0.90807         0.90985
v  Velocity[y]           -0.36816         0.70162      0.00055567      0.00033225
v  Velocity[z]           -0.41974           0.505      -0.0012481      -0.0013657
v  TurbEner             0.0010129        0.014822       0.0032861       0.0033457
v  Dissip              9.2172e-05        0.027578      0.00044958      0.00038907
v  TurbVisc               0.16503          11.376          4.7141          5.2753
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              457:        0.96808E-01

===============================================================


 INSTANT    0.458000000E+03   TIME STEP NUMBER             458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000276E+04
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 :  0.23792E+00 0.13255E+01
   Friction velocity        uet   :  0.14230E-01 0.79002E-01
   Friction velocity        uk    :  0.17431E-01 0.38627E-01
   Dimensionless distance   yplus :  0.42779E+03 0.95285E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60334E+01      58   0.11686E-02   0.19771E-01 
c  VelocityX    0.46302E+04      12   0.69239E-02   0.38287E-03 
c  VelocityY    0.46302E+04      12   0.69239E-02   0.23612E-04 
c  VelocityZ    0.46302E+04      12   0.69239E-02   0.32058E-04 
c  TurbEner     0.59768E+01      13   0.64305E-04   0.10775E-08 
c  Dissip       0.13548E+01      15   0.46559E-03   0.64315E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.71           54518           26778           27273
v  Velocity[x]            0.29312          2.1475         0.90805         0.90983
v  Velocity[y]           -0.38252         0.69299      0.00055077      0.00032987
v  Velocity[z]           -0.42051          0.5123        -0.00125        -0.00137
v  TurbEner             0.0010138        0.014756       0.0032863       0.0033458
v  Dissip              9.2151e-05        0.027677      0.00044978      0.00038919
v  TurbVisc               0.16505          11.357          4.7143          5.2755
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              458:        0.96142E-01

===============================================================


 INSTANT    0.459000000E+03   TIME STEP NUMBER             459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000695E+04
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 :  0.23771E+00 0.12165E+01
   Friction velocity        uet   :  0.14218E-01 0.72510E-01
   Friction velocity        uk    :  0.17439E-01 0.38732E-01
   Dimensionless distance   yplus :  0.42838E+03 0.95247E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59074E+01      61   0.12751E-02   0.19375E-01 
c  VelocityX    0.46303E+04      12   0.66822E-02   0.31437E-03 
c  VelocityY    0.46303E+04      12   0.66822E-02   0.23235E-04 
c  VelocityZ    0.46303E+04      12   0.66822E-02   0.38013E-04 
c  TurbEner     0.59780E+01      13   0.72963E-04   0.10919E-08 
c  Dissip       0.13830E+01      16   0.10786E-02   0.25459E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.81           54534           26778           27272
v  Velocity[x]            0.29267          2.1717         0.90808         0.90985
v  Velocity[y]            -0.3662         0.70142      0.00054295      0.00032003
v  Velocity[z]             -0.422         0.50685      -0.0012574       -0.001375
v  TurbEner             0.0010123        0.014919       0.0032865       0.0033459
v  Dissip              9.2079e-05        0.028212      0.00045011      0.00038939
v  TurbVisc               0.16552           11.36          4.7145          5.2756
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              459:        0.96546E-01

===============================================================


 INSTANT    0.460000000E+03   TIME STEP NUMBER             460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001358E+04
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 :  0.23784E+00 0.13233E+01
   Friction velocity        uet   :  0.14225E-01 0.78876E-01
   Friction velocity        uk    :  0.17427E-01 0.38747E-01
   Dimensionless distance   yplus :  0.42834E+03 0.95237E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60691E+01      62   0.14365E-02   0.19895E-01 
c  VelocityX    0.46302E+04      12   0.66515E-02   0.40959E-03 
c  VelocityY    0.46302E+04      12   0.66515E-02   0.37041E-04 
c  VelocityZ    0.46302E+04      12   0.66515E-02   0.12266E-03 
c  TurbEner     0.59791E+01      13   0.12200E-03   0.15060E-08 
c  Dissip       0.14048E+01      16   0.21502E-02   0.53813E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.21           54543           26778           27272
v  Velocity[x]             0.2927          2.0122         0.90806         0.90983
v  Velocity[y]           -0.38252         0.69408      0.00054935      0.00032715
v  Velocity[z]           -0.41998         0.51115      -0.0012582      -0.0013829
v  TurbEner             0.0010155        0.015572        0.003287       0.0033463
v  Dissip              9.2071e-05        0.029919      0.00045052      0.00038967
v  TurbVisc               0.16558          11.332          4.7147          5.2758
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              460:        0.96815E-01

===============================================================


 INSTANT    0.461000000E+03   TIME STEP NUMBER             461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999578E+04
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 :  0.23757E+00 0.12183E+01
   Friction velocity        uet   :  0.14208E-01 0.72504E-01
   Friction velocity        uk    :  0.17454E-01 0.38725E-01
   Dimensionless distance   yplus :  0.42807E+03 0.95178E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.50741E+01      53   0.10835E-02   0.16638E-01 
c  VelocityX    0.46302E+04      13   0.66597E-02   0.29921E-03 
c  VelocityY    0.46302E+04      13   0.66597E-02   0.28443E-04 
c  VelocityZ    0.46302E+04      13   0.66597E-02   0.49848E-04 
c  TurbEner     0.59785E+01      13   0.12585E-03   0.16864E-08 
c  Dissip       0.13856E+01      16   0.16144E-02   0.37922E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.42           54551           26778           27272
v  Velocity[x]            0.29311          2.0876         0.90806         0.90984
v  Velocity[y]           -0.36816         0.70039      0.00054453      0.00031967
v  Velocity[z]           -0.42079         0.50409       -0.001252      -0.0013711
v  TurbEner             0.0010204        0.014987       0.0032872       0.0033464
v  Dissip              9.2079e-05        0.028821      0.00045051      0.00038966
v  TurbVisc               0.16566          11.326          4.7149           5.276
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              461:        0.96095E-01

===============================================================


 INSTANT    0.462000000E+03   TIME STEP NUMBER             462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999273E+04
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 :  0.23769E+00 0.13257E+01
   Friction velocity        uet   :  0.14216E-01 0.79023E-01
   Friction velocity        uk    :  0.17496E-01 0.38706E-01
   Dimensionless distance   yplus :  0.42955E+03 0.95174E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60116E+01      55   0.14281E-02   0.19712E-01 
c  VelocityX    0.46304E+04      13   0.73403E-02   0.37353E-03 
c  VelocityY    0.46304E+04      13   0.73403E-02   0.23775E-04 
c  VelocityZ    0.46304E+04      13   0.73403E-02   0.35090E-04 
c  TurbEner     0.59794E+01      13   0.64055E-04   0.69557E-09 
c  Dissip       0.13980E+01      14   0.36678E-03   0.35897E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -167.7           54545           26779           27273
v  Velocity[x]            0.29268          2.1436         0.90808         0.90986
v  Velocity[y]           -0.38303         0.69387      0.00054331      0.00032486
v  Velocity[z]           -0.42214         0.51143      -0.0012488      -0.0013705
v  TurbEner             0.0010199        0.014883       0.0032875       0.0033467
v  Dissip              9.2108e-05        0.028779      0.00045071       0.0003898
v  TurbVisc               0.16667          11.356          4.7151          5.2762
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              462:        0.96503E-01

===============================================================


 INSTANT    0.463000000E+03   TIME STEP NUMBER             463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998370E+04
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 :  0.23780E+00 0.12144E+01
   Friction velocity        uet   :  0.14222E-01 0.72304E-01
   Friction velocity        uk    :  0.17492E-01 0.38659E-01
   Dimensionless distance   yplus :  0.42969E+03 0.95230E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62532E+01      70   0.15034E-02   0.20511E-01 
c  VelocityX    0.46304E+04      13   0.72014E-02   0.40798E-03 
c  VelocityY    0.46304E+04      13   0.72014E-02   0.25857E-04 
c  VelocityZ    0.46304E+04      13   0.72014E-02   0.42648E-04 
c  TurbEner     0.59804E+01      13   0.80155E-04   0.12643E-08 
c  Dissip       0.14231E+01      16   0.96028E-03   0.20978E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.25           54520           26779           27274
v  Velocity[x]            0.29278          2.1682         0.90809         0.90987
v  Velocity[y]           -0.36806         0.70244      0.00055405      0.00033283
v  Velocity[z]            -0.4214         0.50714      -0.0012489      -0.0013668
v  TurbEner             0.0010266        0.015019       0.0032878       0.0033469
v  Dissip              9.2109e-05        0.029228      0.00045104      0.00039003
v  TurbVisc               0.16682          11.405          4.7153          5.2764
v  total_pressure           83083      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              463:        0.99347E-01

===============================================================


 INSTANT    0.464000000E+03   TIME STEP NUMBER             464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999538E+04
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 :  0.23794E+00 0.13250E+01
   Friction velocity        uet   :  0.14231E-01 0.78985E-01
   Friction velocity        uk    :  0.17550E-01 0.38733E-01
   Dimensionless distance   yplus :  0.43016E+03 0.95234E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72656E+01      66   0.14232E-02   0.23821E-01 
c  VelocityX    0.46302E+04      12   0.69767E-02   0.40009E-03 
c  VelocityY    0.46302E+04      12   0.69767E-02   0.50388E-04 
c  VelocityZ    0.46302E+04      12   0.69767E-02   0.13519E-03 
c  TurbEner     0.59810E+01      13   0.12595E-03   0.15052E-08 
c  Dissip       0.14435E+01      16   0.19846E-02   0.45520E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -165.72           54529           26779           27274
v  Velocity[x]            0.29275          2.0153         0.90803         0.90981
v  Velocity[y]           -0.38281         0.69244       0.0005592      0.00033568
v  Velocity[z]           -0.42054         0.51394      -0.0012405      -0.0013635
v  TurbEner             0.0010311        0.015631       0.0032882       0.0033473
v  Dissip              9.2091e-05        0.030809      0.00045138      0.00039027
v  TurbVisc               0.16727          11.393          4.7154          5.2765
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              464:        0.98379E-01

===============================================================


 INSTANT    0.465000000E+03   TIME STEP NUMBER             465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000434E+04
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 :  0.23774E+00 0.12165E+01
   Friction velocity        uet   :  0.14219E-01 0.72515E-01
   Friction velocity        uk    :  0.17588E-01 0.38768E-01
   Dimensionless distance   yplus :  0.43145E+03 0.95251E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67237E+01      61   0.13414E-02   0.22060E-01 
c  VelocityX    0.46303E+04      12   0.63156E-02   0.36265E-03 
c  VelocityY    0.46303E+04      12   0.63156E-02   0.66197E-04 
c  VelocityZ    0.46303E+04      12   0.63156E-02   0.59240E-04 
c  TurbEner     0.59798E+01      13   0.12798E-03   0.19480E-08 
c  Dissip       0.14145E+01      16   0.18615E-02   0.50564E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.69           54528           26780           27274
v  Velocity[x]            0.29306          2.0825         0.90806         0.90984
v  Velocity[y]           -0.36661         0.70071      0.00055065      0.00032753
v  Velocity[z]           -0.42112           0.508      -0.0012558      -0.0013765
v  TurbEner             0.0010324        0.015065       0.0032882       0.0033473
v  Dissip              9.2031e-05        0.029548      0.00045125      0.00039018
v  TurbVisc                0.1681           11.34          4.7156          5.2767
v  total_pressure           83082      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              465:        0.97747E-01

===============================================================


 INSTANT    0.466000000E+03   TIME STEP NUMBER             466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999232E+04
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 :  0.23787E+00 0.13243E+01
   Friction velocity        uet   :  0.14228E-01 0.78944E-01
   Friction velocity        uk    :  0.17599E-01 0.38690E-01
   Dimensionless distance   yplus :  0.43209E+03 0.95316E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62965E+01      59   0.13776E-02   0.20657E-01 
c  VelocityX    0.46304E+04      12   0.70193E-02   0.32672E-03 
c  VelocityY    0.46304E+04      12   0.70193E-02   0.35453E-04 
c  VelocityZ    0.46304E+04      12   0.70193E-02   0.28608E-04 
c  TurbEner     0.59802E+01      12   0.64740E-04   0.74630E-09 
c  Dissip       0.14228E+01      13   0.37245E-03   0.26658E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.85           54511           26780           27275
v  Velocity[x]            0.29287          2.1451         0.90806         0.90984
v  Velocity[y]           -0.38273         0.69341      0.00055573      0.00033606
v  Velocity[z]           -0.42083         0.51215      -0.0012375        -0.00136
v  TurbEner             0.0010373        0.014961       0.0032882       0.0033474
v  Dissip              9.2002e-05        0.029372      0.00045138      0.00039028
v  TurbVisc               0.16842          11.327          4.7156          5.2767
v  total_pressure           83077      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              466:        0.96008E-01

===============================================================


 INSTANT    0.467000000E+03   TIME STEP NUMBER             467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998770E+04
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 :  0.23759E+00 0.12235E+01
   Friction velocity        uet   :  0.14212E-01 0.72546E-01
   Friction velocity        uk    :  0.17641E-01 0.38721E-01
   Dimensionless distance   yplus :  0.43226E+03 0.95292E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67991E+01      57   0.13500E-02   0.22281E-01 
c  VelocityX    0.46303E+04      12   0.72697E-02   0.33543E-03 
c  VelocityY    0.46303E+04      12   0.72697E-02   0.36042E-04 
c  VelocityZ    0.46303E+04      12   0.72697E-02   0.40971E-04 
c  TurbEner     0.59804E+01      13   0.72100E-04   0.11698E-08 
c  Dissip       0.14428E+01      15   0.79353E-03   0.14274E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.74           54518           26779           27274
v  Velocity[x]            0.29304          2.1652         0.90805         0.90983
v  Velocity[y]           -0.36803         0.70224      0.00054397      0.00031921
v  Velocity[z]           -0.42046         0.50511      -0.0012492      -0.0013677
v  TurbEner             0.0010428         0.01512       0.0032883       0.0033474
v  Dissip              9.1992e-05        0.029765      0.00045158      0.00039041
v  TurbVisc               0.16859          11.353          4.7156          5.2767
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              467:        0.96236E-01

===============================================================


 INSTANT    0.468000000E+03   TIME STEP NUMBER             468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001510E+04
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 :  0.23724E+00 0.13243E+01
   Friction velocity        uet   :  0.14191E-01 0.78936E-01
   Friction velocity        uk    :  0.17687E-01 0.38760E-01
   Dimensionless distance   yplus :  0.43394E+03 0.95357E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59167E+01      52   0.14821E-02   0.19405E-01 
c  VelocityX    0.46304E+04      12   0.67016E-02   0.44869E-03 
c  VelocityY    0.46304E+04      12   0.67016E-02   0.25035E-04 
c  VelocityZ    0.46304E+04      12   0.67016E-02   0.42923E-04 
c  TurbEner     0.59813E+01      13   0.11522E-03   0.12947E-08 
c  Dissip       0.14620E+01      16   0.19894E-02   0.45861E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.76           54523           26779           27274
v  Velocity[x]            0.29235          2.0155         0.90807         0.90985
v  Velocity[y]           -0.38262         0.69498      0.00054084      0.00032168
v  Velocity[z]           -0.42007         0.51232      -0.0012522      -0.0013736
v  TurbEner             0.0010411        0.015709       0.0032885       0.0033475
v  Dissip              9.2042e-05        0.031347      0.00045191      0.00039065
v  TurbVisc               0.16951          11.319          4.7156          5.2767
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              468:        0.95439E-01

===============================================================


 INSTANT    0.469000000E+03   TIME STEP NUMBER             469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000456E+04
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 :  0.23795E+00 0.12167E+01
   Friction velocity        uet   :  0.14234E-01 0.72532E-01
   Friction velocity        uk    :  0.17673E-01 0.38736E-01
   Dimensionless distance   yplus :  0.43397E+03 0.95347E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60084E+01      56   0.14400E-02   0.19711E-01 
c  VelocityX    0.46303E+04      12   0.64801E-02   0.34264E-03 
c  VelocityY    0.46303E+04      12   0.64801E-02   0.22716E-04 
c  VelocityZ    0.46303E+04      12   0.64801E-02   0.49968E-04 
c  TurbEner     0.59800E+01      13   0.13809E-03   0.19689E-08 
c  Dissip       0.14308E+01      16   0.21112E-02   0.60740E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.77           54507           26779           27273
v  Velocity[x]            0.29273          2.0894         0.90806         0.90983
v  Velocity[y]           -0.36672         0.70183       0.0005503      0.00032667
v  Velocity[z]           -0.42119         0.50641      -0.0012471      -0.0013657
v  TurbEner             0.0010458         0.01504       0.0032885       0.0033476
v  Dissip              9.2018e-05        0.029878      0.00045177      0.00039055
v  TurbVisc                0.1694          11.325          4.7156          5.2768
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              469:        0.95849E-01

===============================================================


 INSTANT    0.470000000E+03   TIME STEP NUMBER             470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001057E+04
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 :  0.23771E+00 0.13254E+01
   Friction velocity        uet   :  0.14220E-01 0.79004E-01
   Friction velocity        uk    :  0.17713E-01 0.38760E-01
   Dimensionless distance   yplus :  0.43413E+03 0.95331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57229E+01      53   0.12389E-02   0.18772E-01 
c  VelocityX    0.46302E+04      12   0.69193E-02   0.27186E-03 
c  VelocityY    0.46302E+04      12   0.69193E-02   0.57175E-04 
c  VelocityZ    0.46302E+04      12   0.69193E-02   0.13467E-03 
c  TurbEner     0.59798E+01      12   0.59991E-04   0.86767E-09 
c  Dissip       0.14376E+01      13   0.27658E-03   0.18505E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.47           54533           26779           27273
v  Velocity[x]            0.29323          2.1423         0.90804         0.90982
v  Velocity[y]           -0.38238         0.69534      0.00055973       0.0003351
v  Velocity[z]            -0.4205         0.51137      -0.0012303      -0.0013536
v  TurbEner             0.0010476        0.015017       0.0032884       0.0033475
v  Dissip              9.2032e-05        0.029751      0.00045178      0.00039054
v  TurbVisc                0.1695          11.364          4.7157          5.2768
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              470:        0.95190E-01

===============================================================


 INSTANT    0.471000000E+03   TIME STEP NUMBER             471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998582E+04
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 :  0.23796E+00 0.12242E+01
   Friction velocity        uet   :  0.14235E-01 0.72356E-01
   Friction velocity        uk    :  0.17728E-01 0.38791E-01
   Dimensionless distance   yplus :  0.43500E+03 0.95335E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56922E+01      56   0.13685E-02   0.18671E-01 
c  VelocityX    0.46303E+04      13   0.72366E-02   0.30478E-03 
c  VelocityY    0.46303E+04      13   0.72366E-02   0.30082E-04 
c  VelocityZ    0.46303E+04      13   0.72366E-02   0.60142E-04 
c  TurbEner     0.59808E+01      13   0.82862E-04   0.10002E-08 
c  Dissip       0.14604E+01      16   0.10675E-02   0.27477E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.93           54521           26779           27273
v  Velocity[x]            0.29266          2.1762         0.90806         0.90983
v  Velocity[y]           -0.36703         0.70308      0.00055573      0.00032996
v  Velocity[z]           -0.42166         0.50499      -0.0012497      -0.0013721
v  TurbEner             0.0010458        0.015161       0.0032884       0.0033475
v  Dissip              9.2047e-05         0.03012      0.00045197      0.00039067
v  TurbVisc               0.16995           11.35          4.7157          5.2768
v  total_pressure           83083      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              471:        0.96672E-01

===============================================================


 INSTANT    0.472000000E+03   TIME STEP NUMBER             472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000773E+04
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 :  0.23799E+00 0.13259E+01
   Friction velocity        uet   :  0.14237E-01 0.79037E-01
   Friction velocity        uk    :  0.17713E-01 0.38765E-01
   Dimensionless distance   yplus :  0.43508E+03 0.95328E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63353E+01      56   0.14434E-02   0.20777E-01 
c  VelocityX    0.46303E+04      12   0.77686E-02   0.42429E-03 
c  VelocityY    0.46303E+04      12   0.77686E-02   0.26563E-04 
c  VelocityZ    0.46303E+04      12   0.77686E-02   0.36607E-04 
c  TurbEner     0.59823E+01      13   0.74941E-04   0.11215E-08 
c  Dissip       0.14950E+01      16   0.11082E-02   0.21344E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.08           54524           26779           27273
v  Velocity[x]            0.29261          2.2048         0.90806         0.90985
v  Velocity[y]           -0.38249         0.69243      0.00055906      0.00033768
v  Velocity[z]           -0.42249         0.51194      -0.0012375      -0.0013594
v  TurbEner             0.0010473        0.015382       0.0032887       0.0033477
v  Dissip              9.2089e-05        0.030873      0.00045229      0.00039089
v  TurbVisc               0.16985          11.354          4.7157          5.2769
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              472:        0.95911E-01

===============================================================


 INSTANT    0.473000000E+03   TIME STEP NUMBER             473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001560E+04
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 :  0.23742E+00 0.12175E+01
   Friction velocity        uet   :  0.14202E-01 0.72576E-01
   Friction velocity        uk    :  0.17725E-01 0.38788E-01
   Dimensionless distance   yplus :  0.43458E+03 0.95345E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65355E+01      67   0.14073E-02   0.21412E-01 
c  VelocityX    0.46302E+04      12   0.74780E-02   0.50133E-03 
c  VelocityY    0.46302E+04      12   0.74780E-02   0.26071E-04 
c  VelocityZ    0.46302E+04      12   0.74780E-02   0.54131E-04 
c  TurbEner     0.59822E+01      13   0.11912E-03   0.15335E-08 
c  Dissip       0.15148E+01      16   0.22251E-02   0.59358E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.18           54510           26778           27273
v  Velocity[x]            0.29295          2.0281         0.90805         0.90983
v  Velocity[y]            -0.3669         0.69966      0.00054939      0.00032694
v  Velocity[z]           -0.41918         0.50583      -0.0012594      -0.0013801
v  TurbEner             0.0010487        0.015979       0.0032888       0.0033478
v  Dissip              9.2094e-05        0.032667      0.00045255      0.00039107
v  TurbVisc               0.16956           11.33          4.7158           5.277
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              473:        0.98774E-01

===============================================================


 INSTANT    0.474000000E+03   TIME STEP NUMBER             474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000532E+04
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 :  0.23765E+00 0.13238E+01
   Friction velocity        uet   :  0.14216E-01 0.78909E-01
   Friction velocity        uk    :  0.17737E-01 0.38816E-01
   Dimensionless distance   yplus :  0.43546E+03 0.95329E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63513E+01      59   0.14868E-02   0.20828E-01 
c  VelocityX    0.46303E+04      12   0.70665E-02   0.36064E-03 
c  VelocityY    0.46303E+04      12   0.70665E-02   0.57551E-04 
c  VelocityZ    0.46303E+04      12   0.70665E-02   0.13083E-03 
c  TurbEner     0.59814E+01      14   0.13871E-03   0.22392E-08 
c  Dissip       0.14918E+01      16   0.17883E-02   0.52751E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.65           54523           26779           27273
v  Velocity[x]             0.2928           2.101         0.90806         0.90984
v  Velocity[y]           -0.38285         0.69472      0.00055356      0.00033233
v  Velocity[z]           -0.42121         0.51051      -0.0012374      -0.0013626
v  TurbEner             0.0010441        0.015387       0.0032886       0.0033476
v  Dissip              9.2084e-05        0.031531       0.0004524      0.00039096
v  TurbVisc                  0.17          11.325          4.7159           5.277
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              474:        0.96270E-01

===============================================================


 INSTANT    0.475000000E+03   TIME STEP NUMBER             475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998648E+04
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 :  0.23774E+00 0.12125E+01
   Friction velocity        uet   :  0.14222E-01 0.72275E-01
   Friction velocity        uk    :  0.17699E-01 0.38732E-01
   Dimensionless distance   yplus :  0.43492E+03 0.95311E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63206E+01      56   0.14640E-02   0.20725E-01 
c  VelocityX    0.46302E+04      13   0.65191E-02   0.38222E-03 
c  VelocityY    0.46302E+04      13   0.65191E-02   0.32500E-04 
c  VelocityZ    0.46302E+04      13   0.65191E-02   0.59608E-04 
c  TurbEner     0.59817E+01      13   0.74528E-04   0.10973E-08 
c  Dissip       0.15053E+01      14   0.43799E-03   0.54289E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.23           54511           26778           27273
v  Velocity[x]            0.29268          2.1488         0.90806         0.90984
v  Velocity[y]           -0.36741         0.70395      0.00055887      0.00033578
v  Velocity[z]           -0.42012         0.50444      -0.0012416      -0.0013632
v  TurbEner              0.001046        0.015289       0.0032887       0.0033477
v  Dissip              9.2086e-05        0.031547       0.0004525      0.00039103
v  TurbVisc               0.16955          11.354          4.7158           5.277
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              475:        0.96266E-01

===============================================================


 INSTANT    0.476000000E+03   TIME STEP NUMBER             476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999975E+04
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 :  0.23796E+00 0.13248E+01
   Friction velocity        uet   :  0.14236E-01 0.78970E-01
   Friction velocity        uk    :  0.17714E-01 0.38748E-01
   Dimensionless distance   yplus :  0.43460E+03 0.95293E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59057E+01      54   0.12211E-02   0.19361E-01 
c  VelocityX    0.46303E+04      12   0.68978E-02   0.36648E-03 
c  VelocityY    0.46303E+04      12   0.68978E-02   0.25139E-04 
c  VelocityZ    0.46303E+04      12   0.68978E-02   0.36137E-04 
c  TurbEner     0.59819E+01      12   0.73093E-04   0.95703E-09 
c  Dissip       0.15335E+01      15   0.89464E-03   0.19113E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.86           54513           26779           27273
v  Velocity[x]            0.29293          2.1883         0.90805         0.90983
v  Velocity[y]           -0.38224         0.69166      0.00055082      0.00032936
v  Velocity[z]           -0.42073         0.51197      -0.0012394      -0.0013608
v  TurbEner             0.0010453        0.015304       0.0032888       0.0033477
v  Dissip              9.2095e-05        0.031929      0.00045274      0.00039118
v  TurbVisc               0.16936          11.336          4.7158           5.277
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              476:        0.95620E-01

===============================================================


 INSTANT    0.477000000E+03   TIME STEP NUMBER             477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999439E+04
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 :  0.23773E+00 0.12179E+01
   Friction velocity        uet   :  0.14223E-01 0.72593E-01
   Friction velocity        uk    :  0.17708E-01 0.38779E-01
   Dimensionless distance   yplus :  0.43500E+03 0.95278E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57078E+01      57   0.14926E-02   0.18728E-01 
c  VelocityX    0.46302E+04      12   0.70992E-02   0.38325E-03 
c  VelocityY    0.46302E+04      12   0.70992E-02   0.24141E-04 
c  VelocityZ    0.46302E+04      12   0.70992E-02   0.47522E-04 
c  TurbEner     0.59819E+01      13   0.10623E-03   0.10161E-08 
c  Dissip       0.15485E+01      16   0.19586E-02   0.44486E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.92           54515           26779           27273
v  Velocity[x]            0.29271          2.0187         0.90806         0.90983
v  Velocity[y]            -0.3661         0.70063      0.00054884       0.0003272
v  Velocity[z]           -0.42247         0.50656      -0.0012579      -0.0013796
v  TurbEner             0.0010407        0.015778       0.0032887       0.0033476
v  Dissip              9.2103e-05        0.033485        0.000453      0.00039138
v  TurbVisc               0.16952          11.324          4.7158          5.2769
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              477:        0.95685E-01

===============================================================


 INSTANT    0.478000000E+03   TIME STEP NUMBER             478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000988E+04
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 :  0.23765E+00 0.13239E+01
   Friction velocity        uet   :  0.14218E-01 0.78910E-01
   Friction velocity        uk    :  0.17670E-01 0.38809E-01
   Dimensionless distance   yplus :  0.43453E+03 0.95294E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64540E+01      55   0.15455E-02   0.21163E-01 
c  VelocityX    0.46302E+04      12   0.64794E-02   0.38336E-03 
c  VelocityY    0.46302E+04      12   0.64794E-02   0.54377E-04 
c  VelocityZ    0.46302E+04      12   0.64794E-02   0.12960E-03 
c  TurbEner     0.59803E+01      14   0.15262E-03   0.25178E-08 
c  Dissip       0.15159E+01      16   0.22179E-02   0.75639E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.16           54518           26779           27273
v  Velocity[x]            0.29253          2.0934         0.90805         0.90983
v  Velocity[y]           -0.38229         0.69463      0.00056337      0.00034174
v  Velocity[z]           -0.41988          0.5111      -0.0012254       -0.001349
v  TurbEner             0.0010401        0.015128       0.0032884       0.0033475
v  Dissip              9.2081e-05        0.032062      0.00045279      0.00039124
v  TurbVisc                0.1691           11.36          4.7156          5.2767
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              478:        0.95390E-01

===============================================================


 INSTANT    0.479000000E+03   TIME STEP NUMBER             479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999511E+04
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 :  0.23756E+00 0.12168E+01
   Friction velocity        uet   :  0.14214E-01 0.72536E-01
   Friction velocity        uk    :  0.17665E-01 0.38827E-01
   Dimensionless distance   yplus :  0.43355E+03 0.95267E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57188E+01      57   0.12614E-02   0.18754E-01 
c  VelocityX    0.46301E+04      12   0.65073E-02   0.32026E-03 
c  VelocityY    0.46301E+04      12   0.65073E-02   0.34367E-04 
c  VelocityZ    0.46301E+04      12   0.65073E-02   0.56416E-04 
c  TurbEner     0.59798E+01      12   0.69266E-04   0.92312E-09 
c  Dissip       0.15210E+01      14   0.49780E-03   0.47855E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.09           54509           26778           27272
v  Velocity[x]            0.29305          2.1428         0.90805         0.90982
v  Velocity[y]           -0.36769         0.70327      0.00055343      0.00032924
v  Velocity[z]            -0.4197         0.50417      -0.0012451      -0.0013645
v  TurbEner             0.0010403        0.015002       0.0032883       0.0033474
v  Dissip              9.2082e-05        0.031829      0.00045277      0.00039122
v  TurbVisc               0.16857          11.348          4.7154          5.2766
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              479:        0.95481E-01

===============================================================


 INSTANT    0.480000000E+03   TIME STEP NUMBER             480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002032E+04
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 :  0.23770E+00 0.13242E+01
   Friction velocity        uet   :  0.14223E-01 0.78931E-01
   Friction velocity        uk    :  0.17666E-01 0.38811E-01
   Dimensionless distance   yplus :  0.43417E+03 0.95276E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58205E+01      53   0.13705E-02   0.19086E-01 
c  VelocityX    0.46302E+04      12   0.73387E-02   0.30570E-03 
c  VelocityY    0.46302E+04      12   0.73387E-02   0.22646E-04 
c  VelocityZ    0.46302E+04      12   0.73387E-02   0.28079E-04 
c  TurbEner     0.59806E+01      12   0.65014E-04   0.61560E-09 
c  Dissip       0.15398E+01      15   0.64854E-03   0.10311E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.42           54518           26778           27272
v  Velocity[x]            0.29284          2.1833         0.90805         0.90983
v  Velocity[y]           -0.38247         0.69591      0.00055088      0.00033214
v  Velocity[z]            -0.4221         0.51173      -0.0012436      -0.0013681
v  TurbEner             0.0010341        0.015015       0.0032882       0.0033473
v  Dissip               9.205e-05        0.032004      0.00045287      0.00039129
v  TurbVisc               0.16891          11.353          4.7154          5.2766
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              480:        0.94940E-01

===============================================================


 INSTANT    0.481000000E+03   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001430E+04
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 :  0.23764E+00 0.12171E+01
   Friction velocity        uet   :  0.14220E-01 0.72550E-01
   Friction velocity        uk    :  0.17614E-01 0.38696E-01
   Dimensionless distance   yplus :  0.43325E+03 0.95290E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63877E+01      55   0.15475E-02   0.20948E-01 
c  VelocityX    0.46301E+04      12   0.74232E-02   0.45743E-03 
c  VelocityY    0.46301E+04      12   0.74232E-02   0.22908E-04 
c  VelocityZ    0.46301E+04      12   0.74232E-02   0.43385E-04 
c  TurbEner     0.59804E+01      13   0.10438E-03   0.11924E-08 
c  Dissip       0.15493E+01      15   0.18138E-02   0.34870E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.43           54497           26778           27272
v  Velocity[x]             0.2926          2.0141         0.90805         0.90982
v  Velocity[y]           -0.36656         0.70123      0.00055395      0.00033384
v  Velocity[z]           -0.42058         0.50604      -0.0012457      -0.0013665
v  TurbEner             0.0010348        0.015502       0.0032881       0.0033472
v  Dissip              9.2054e-05        0.033436      0.00045301       0.0003914
v  TurbVisc                0.1683          11.332          4.7152          5.2764
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              481:        0.95145E-01

===============================================================


 INSTANT    0.482000000E+03   TIME STEP NUMBER             482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000732E+04
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 :  0.23785E+00 0.13259E+01
   Friction velocity        uet   :  0.14233E-01 0.79022E-01
   Friction velocity        uk    :  0.17619E-01 0.38700E-01
   Dimensionless distance   yplus :  0.43259E+03 0.95291E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71759E+01      75   0.14584E-02   0.23514E-01 
c  VelocityX    0.46300E+04      12   0.62462E-02   0.41411E-03 
c  VelocityY    0.46300E+04      12   0.62462E-02   0.51105E-04 
c  VelocityZ    0.46300E+04      12   0.62462E-02   0.13328E-03 
c  TurbEner     0.59786E+01      14   0.14918E-03   0.22814E-08 
c  Dissip       0.15115E+01      17   0.25241E-02   0.89241E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.33           54525           26777           27271
v  Velocity[x]            0.29278          2.0949         0.90803         0.90981
v  Velocity[y]           -0.38224         0.69287      0.00055972      0.00033902
v  Velocity[z]           -0.42075         0.51098      -0.0012334      -0.0013575
v  TurbEner             0.0010336         0.01486       0.0032877        0.003347
v  Dissip              9.2021e-05        0.031784      0.00045265      0.00039115
v  TurbVisc                 0.168          11.326          4.7151          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              482:        0.10054E+00

===============================================================


 INSTANT    0.483000000E+03   TIME STEP NUMBER             483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000912E+04
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 :  0.23765E+00 0.12160E+01
   Friction velocity        uet   :  0.14222E-01 0.72479E-01
   Friction velocity        uk    :  0.17609E-01 0.38751E-01
   Dimensionless distance   yplus :  0.43276E+03 0.95297E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68314E+01      67   0.15046E-02   0.22406E-01 
c  VelocityX    0.46301E+04      12   0.66145E-02   0.34162E-03 
c  VelocityY    0.46301E+04      12   0.66145E-02   0.62798E-04 
c  VelocityZ    0.46301E+04      12   0.66145E-02   0.60150E-04 
c  TurbEner     0.59784E+01      13   0.67163E-04   0.93314E-09 
c  Dissip       0.15025E+01      14   0.78269E-03   0.74509E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.5           54509           26777           27271
v  Velocity[x]              0.293          2.1382         0.90806         0.90984
v  Velocity[y]           -0.36696         0.70124      0.00054654      0.00032355
v  Velocity[z]           -0.42207         0.50473      -0.0012475       -0.001366
v  TurbEner             0.0010293        0.014744       0.0032874       0.0033467
v  Dissip              9.2066e-05        0.031252       0.0004525      0.00039104
v  TurbVisc                0.1681          11.353          4.7149          5.2761
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              483:        0.98105E-01

===============================================================


 INSTANT    0.484000000E+03   TIME STEP NUMBER             484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000799E+04
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 :  0.23765E+00 0.13233E+01
   Friction velocity        uet   :  0.14223E-01 0.78881E-01
   Friction velocity        uk    :  0.17572E-01 0.38791E-01
   Dimensionless distance   yplus :  0.43226E+03 0.95261E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66579E+01      57   0.14747E-02   0.21830E-01 
c  VelocityX    0.46300E+04      12   0.72540E-02   0.33882E-03 
c  VelocityY    0.46300E+04      12   0.72540E-02   0.41187E-04 
c  VelocityZ    0.46300E+04      12   0.72540E-02   0.28551E-04 
c  TurbEner     0.59793E+01      12   0.70243E-04   0.83759E-09 
c  Dissip       0.15173E+01      14   0.52287E-03   0.67378E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.71           54513           26777           27271
v  Velocity[x]            0.29269          2.1837         0.90804         0.90982
v  Velocity[y]           -0.38244         0.69385      0.00055829      0.00033934
v  Velocity[z]           -0.41973         0.51173      -0.0012289      -0.0013507
v  TurbEner             0.0010289        0.014838       0.0032873       0.0033467
v  Dissip              9.2112e-05        0.031377      0.00045251      0.00039104
v  TurbVisc               0.16773          11.336          4.7148           5.276
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              484:        0.95990E-01

===============================================================


 INSTANT    0.485000000E+03   TIME STEP NUMBER             485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998516E+04
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 :  0.23736E+00 0.12161E+01
   Friction velocity        uet   :  0.14206E-01 0.72498E-01
   Friction velocity        uk    :  0.17569E-01 0.38714E-01
   Dimensionless distance   yplus :  0.43127E+03 0.95299E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67346E+01      58   0.13674E-02   0.22078E-01 
c  VelocityX    0.46300E+04      12   0.74292E-02   0.41969E-03 
c  VelocityY    0.46300E+04      12   0.74292E-02   0.39532E-04 
c  VelocityZ    0.46300E+04      12   0.74292E-02   0.47984E-04 
c  TurbEner     0.59788E+01      13   0.12447E-03   0.15573E-08 
c  Dissip       0.15262E+01      16   0.18751E-02   0.37276E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.57           54501           26777           27271
v  Velocity[x]              0.293          2.0106         0.90805         0.90983
v  Velocity[y]           -0.36691         0.70047      0.00055063      0.00032749
v  Velocity[z]           -0.42053         0.50568       -0.001249      -0.0013671
v  TurbEner             0.0010295        0.015422       0.0032871       0.0033465
v  Dissip              9.2134e-05        0.032839      0.00045256      0.00039109
v  TurbVisc               0.16721          11.344          4.7147          5.2759
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              485:        0.95853E-01

===============================================================


 INSTANT    0.486000000E+03   TIME STEP NUMBER             486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001231E+04
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 :  0.23767E+00 0.13252E+01
   Friction velocity        uet   :  0.14225E-01 0.78993E-01
   Friction velocity        uk    :  0.17574E-01 0.38724E-01
   Dimensionless distance   yplus :  0.43194E+03 0.95325E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70174E+01      73   0.14995E-02   0.23009E-01 
c  VelocityX    0.46300E+04      13   0.69931E-02   0.31563E-03 
c  VelocityY    0.46300E+04      13   0.69931E-02   0.41676E-04 
c  VelocityZ    0.46300E+04      13   0.69931E-02   0.11395E-03 
c  TurbEner     0.59779E+01      14   0.13499E-03   0.20258E-08 
c  Dissip       0.14923E+01      17   0.22714E-02   0.75089E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.6           54520           26777           27271
v  Velocity[x]            0.29282          2.0934         0.90804         0.90981
v  Velocity[y]           -0.38278         0.69395      0.00054933      0.00032818
v  Velocity[z]           -0.42023         0.51051      -0.0012438      -0.0013669
v  TurbEner             0.0010238        0.014865       0.0032868       0.0033463
v  Dissip              9.2133e-05        0.031395      0.00045226      0.00039088
v  TurbVisc               0.16754          11.381          4.7145          5.2757
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              486:        0.10054E+00

===============================================================


 INSTANT    0.487000000E+03   TIME STEP NUMBER             487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000211E+04
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 :  0.23827E+00 0.12144E+01
   Friction velocity        uet   :  0.14261E-01 0.72308E-01
   Friction velocity        uk    :  0.17525E-01 0.38646E-01
   Dimensionless distance   yplus :  0.43107E+03 0.95270E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62405E+01      59   0.12733E-02   0.20467E-01 
c  VelocityX    0.46300E+04      12   0.75934E-02   0.34868E-03 
c  VelocityY    0.46300E+04      12   0.75934E-02   0.33198E-04 
c  VelocityZ    0.46300E+04      12   0.75934E-02   0.50393E-04 
c  TurbEner     0.59779E+01      13   0.61631E-04   0.78669E-09 
c  Dissip       0.14890E+01      14   0.64441E-03   0.52096E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.83           54534           26776           27270
v  Velocity[x]            0.29256          2.1434         0.90807         0.90985
v  Velocity[y]           -0.36734         0.70259      0.00054665      0.00032223
v  Velocity[z]           -0.42136          0.5043      -0.0012615      -0.0013793
v  TurbEner             0.0010243        0.014748       0.0032867       0.0033462
v  Dissip              9.2146e-05        0.030975      0.00045214      0.00039079
v  TurbVisc               0.16689          11.364          4.7144          5.2757
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              487:        0.95778E-01

===============================================================


 INSTANT    0.488000000E+03   TIME STEP NUMBER             488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000199E+04
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 :  0.23761E+00 0.13251E+01
   Friction velocity        uet   :  0.14222E-01 0.78988E-01
   Friction velocity        uk    :  0.17529E-01 0.38697E-01
   Dimensionless distance   yplus :  0.43039E+03 0.95317E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61873E+01      60   0.11819E-02   0.20268E-01 
c  VelocityX    0.46300E+04      12   0.75590E-02   0.37013E-03 
c  VelocityY    0.46300E+04      12   0.75590E-02   0.22730E-04 
c  VelocityZ    0.46300E+04      12   0.75590E-02   0.31031E-04 
c  TurbEner     0.59792E+01      13   0.73533E-04   0.97920E-09 
c  Dissip       0.15059E+01      15   0.65274E-03   0.10114E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.95           54546           26777           27271
v  Velocity[x]            0.29295          2.1816         0.90806         0.90984
v  Velocity[y]           -0.38216         0.69274      0.00053931      0.00031897
v  Velocity[z]           -0.42135         0.51187      -0.0012549      -0.0013751
v  TurbEner             0.0010223         0.01484       0.0032868       0.0033463
v  Dissip              9.2124e-05        0.031156      0.00045223      0.00039085
v  TurbVisc                0.1665          11.366          4.7144          5.2756
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              488:        0.95902E-01

===============================================================


 INSTANT    0.489000000E+03   TIME STEP NUMBER             489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999255E+04
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 :  0.23757E+00 0.12171E+01
   Friction velocity        uet   :  0.14219E-01 0.72552E-01
   Friction velocity        uk    :  0.17513E-01 0.38776E-01
   Dimensionless distance   yplus :  0.43039E+03 0.95350E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69413E+01      62   0.15728E-02   0.22763E-01 
c  VelocityX    0.46300E+04      12   0.72478E-02   0.43871E-03 
c  VelocityY    0.46300E+04      12   0.72478E-02   0.40324E-04 
c  VelocityZ    0.46300E+04      12   0.72478E-02   0.44058E-04 
c  TurbEner     0.59800E+01      14   0.12331E-03   0.17193E-08 
c  Dissip       0.15152E+01      16   0.18451E-02   0.36080E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.51           54539           26777           27271
v  Velocity[x]            0.29273          2.0092         0.90808         0.90986
v  Velocity[y]           -0.36606         0.70005      0.00054549      0.00032636
v  Velocity[z]            -0.4217         0.50656      -0.0012683      -0.0013858
v  TurbEner             0.0010177        0.015398        0.003287       0.0033464
v  Dissip              9.2134e-05        0.032594      0.00045238      0.00039096
v  TurbVisc               0.16643          11.341          4.7144          5.2756
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              489:        0.97292E-01

===============================================================


 INSTANT    0.490000000E+03   TIME STEP NUMBER             490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999796E+04
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 :  0.23791E+00 0.13244E+01
   Friction velocity        uet   :  0.14240E-01 0.78948E-01
   Friction velocity        uk    :  0.17473E-01 0.38802E-01
   Dimensionless distance   yplus :  0.42982E+03 0.95363E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73020E+01      71   0.16283E-02   0.23941E-01 
c  VelocityX    0.46300E+04      12   0.68131E-02   0.44701E-03 
c  VelocityY    0.46300E+04      12   0.68131E-02   0.53581E-04 
c  VelocityZ    0.46300E+04      12   0.68131E-02   0.12590E-03 
c  TurbEner     0.59795E+01      14   0.13620E-03   0.25202E-08 
c  Dissip       0.14834E+01      17   0.22278E-02   0.72225E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.64           54515           26777           27271
v  Velocity[x]            0.29275          2.0931         0.90805         0.90983
v  Velocity[y]            -0.3823         0.69298      0.00056324      0.00034445
v  Velocity[z]           -0.42067         0.51104      -0.0012431      -0.0013657
v  TurbEner             0.0010171         0.01484        0.003287       0.0033464
v  Dissip              9.2119e-05        0.031171      0.00045212      0.00039079
v  TurbVisc               0.16587          11.329          4.7143          5.2755
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              490:        0.99216E-01

===============================================================


 INSTANT    0.491000000E+03   TIME STEP NUMBER             491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999520E+04
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 :  0.23723E+00 0.12168E+01
   Friction velocity        uet   :  0.14200E-01 0.72536E-01
   Friction velocity        uk    :  0.17468E-01 0.38737E-01
   Dimensionless distance   yplus :  0.42887E+03 0.95400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59773E+01      56   0.13438E-02   0.19591E-01 
c  VelocityX    0.46299E+04      12   0.61788E-02   0.39235E-03 
c  VelocityY    0.46299E+04      12   0.61788E-02   0.35502E-04 
c  VelocityZ    0.46299E+04      12   0.61788E-02   0.54605E-04 
c  TurbEner     0.59786E+01      13   0.71531E-04   0.11415E-08 
c  Dissip       0.14800E+01      14   0.65294E-03   0.55676E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.6           54522           26777           27271
v  Velocity[x]             0.2932          2.1416         0.90805         0.90984
v  Velocity[y]            -0.3677         0.70151      0.00055227      0.00032943
v  Velocity[z]           -0.41947         0.50413      -0.0012513      -0.0013676
v  TurbEner             0.0010176        0.014729       0.0032869       0.0033464
v  Dissip              9.2169e-05        0.030744      0.00045206      0.00039076
v  TurbVisc               0.16543          11.363          4.7142          5.2755
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              491:        0.95645E-01

===============================================================


 INSTANT    0.492000000E+03   TIME STEP NUMBER             492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002274E+04
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 :  0.23803E+00 0.13241E+01
   Friction velocity        uet   :  0.14248E-01 0.78924E-01
   Friction velocity        uk    :  0.17472E-01 0.38768E-01
   Dimensionless distance   yplus :  0.42951E+03 0.95357E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56609E+01      53   0.11947E-02   0.18563E-01 
c  VelocityX    0.46300E+04      12   0.66668E-02   0.30702E-03 
c  VelocityY    0.46300E+04      12   0.66668E-02   0.21937E-04 
c  VelocityZ    0.46300E+04      12   0.66668E-02   0.32909E-04 
c  TurbEner     0.59796E+01      13   0.75927E-04   0.94234E-09 
c  Dissip       0.14953E+01      15   0.63535E-03   0.97848E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.75           54532           26776           27270
v  Velocity[x]            0.29259          2.1825         0.90805         0.90983
v  Velocity[y]           -0.38247         0.69446      0.00054935      0.00033069
v  Velocity[z]           -0.42179         0.51167      -0.0012509      -0.0013716
v  TurbEner             0.0010122        0.014818       0.0032869       0.0033464
v  Dissip              9.2198e-05        0.030872       0.0004521      0.00039078
v  TurbVisc               0.16574          11.333          4.7141          5.2753
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              492:        0.95457E-01

===============================================================


 INSTANT    0.493000000E+03   TIME STEP NUMBER             493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001383E+04
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 :  0.23786E+00 0.12166E+01
   Friction velocity        uet   :  0.14238E-01 0.72523E-01
   Friction velocity        uk    :  0.17426E-01 0.38735E-01
   Dimensionless distance   yplus :  0.42866E+03 0.95347E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61285E+01      64   0.13573E-02   0.20099E-01 
c  VelocityX    0.46300E+04      12   0.69656E-02   0.36368E-03 
c  VelocityY    0.46300E+04      12   0.69656E-02   0.37142E-04 
c  VelocityZ    0.46300E+04      12   0.69656E-02   0.33273E-04 
c  TurbEner     0.59796E+01      13   0.11695E-03   0.13138E-08 
c  Dissip       0.15036E+01      16   0.18164E-02   0.34450E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.26           54541           26776           27271
v  Velocity[x]            0.29274          2.0093         0.90807         0.90984
v  Velocity[y]           -0.36659          0.7011      0.00054717       0.0003217
v  Velocity[z]           -0.42214         0.50596      -0.0012598      -0.0013789
v  TurbEner              0.001014        0.015389       0.0032868       0.0033464
v  Dissip              9.2156e-05        0.032289      0.00045221      0.00039088
v  TurbVisc               0.16505          11.333           4.714          5.2753
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              493:        0.97516E-01

===============================================================


 INSTANT    0.494000000E+03   TIME STEP NUMBER             494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999103E+04
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 :  0.23761E+00 0.13255E+01
   Friction velocity        uet   :  0.14223E-01 0.79005E-01
   Friction velocity        uk    :  0.17441E-01 0.38786E-01
   Dimensionless distance   yplus :  0.42817E+03 0.95355E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64396E+01      57   0.12554E-02   0.21104E-01 
c  VelocityX    0.46299E+04      12   0.72764E-02   0.35763E-03 
c  VelocityY    0.46299E+04      12   0.72764E-02   0.38843E-04 
c  VelocityZ    0.46299E+04      12   0.72764E-02   0.56865E-04 
c  TurbEner     0.59789E+01      13   0.12396E-03   0.17040E-08 
c  Dissip       0.14704E+01      16   0.21296E-02   0.67088E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.52           54551           26776           27271
v  Velocity[x]            0.29291          2.0906         0.90805         0.90983
v  Velocity[y]            -0.3823         0.69448       0.0005434      0.00032339
v  Velocity[z]           -0.41982         0.51103      -0.0012451      -0.0013669
v  TurbEner              0.001014        0.014855       0.0032866       0.0033463
v  Dissip              9.2182e-05        0.030951      0.00045195       0.0003907
v  TurbVisc                0.1649          11.366          4.7138          5.2752
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              494:        0.96077E-01

===============================================================


 INSTANT    0.495000000E+03   TIME STEP NUMBER             495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000941E+04
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 :  0.23761E+00 0.12137E+01
   Friction velocity        uet   :  0.14222E-01 0.72349E-01
   Friction velocity        uk    :  0.17442E-01 0.38801E-01
   Dimensionless distance   yplus :  0.42855E+03 0.95294E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58763E+01      55   0.12469E-02   0.19265E-01 
c  VelocityX    0.46300E+04      13   0.67837E-02   0.35025E-03 
c  VelocityY    0.46300E+04      13   0.67837E-02   0.30790E-04 
c  VelocityZ    0.46300E+04      13   0.67837E-02   0.42754E-04 
c  TurbEner     0.59792E+01      12   0.63197E-04   0.69179E-09 
c  Dissip       0.14738E+01      14   0.57872E-03   0.43249E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.06           54553           26776           27270
v  Velocity[x]            0.29258          2.1421         0.90806         0.90984
v  Velocity[y]           -0.36693         0.70286       0.0005429      0.00032026
v  Velocity[z]            -0.4209         0.50473      -0.0012626      -0.0013822
v  TurbEner             0.0010114        0.014749       0.0032867       0.0033463
v  Dissip              9.2194e-05        0.030591      0.00045193      0.00039069
v  TurbVisc               0.16511          11.348          4.7137          5.2751
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              495:        0.96140E-01

===============================================================


 INSTANT    0.496000000E+03   TIME STEP NUMBER             496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001837E+04
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 :  0.23776E+00 0.13257E+01
   Friction velocity        uet   :  0.14231E-01 0.79022E-01
   Friction velocity        uk    :  0.17419E-01 0.38786E-01
   Dimensionless distance   yplus :  0.42833E+03 0.95343E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65695E+01      55   0.13332E-02   0.21528E-01 
c  VelocityX    0.46300E+04      12   0.72733E-02   0.38085E-03 
c  VelocityY    0.46300E+04      12   0.72733E-02   0.36053E-04 
c  VelocityZ    0.46300E+04      12   0.72733E-02   0.84208E-04 
c  TurbEner     0.59803E+01      13   0.74880E-04   0.91099E-09 
c  Dissip       0.14914E+01      15   0.70393E-03   0.11984E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.28           54544           26776           27270
v  Velocity[x]            0.29279           2.184         0.90808         0.90986
v  Velocity[y]           -0.38243         0.69302      0.00055182      0.00033357
v  Velocity[z]           -0.42058         0.51171      -0.0012425      -0.0013655
v  TurbEner             0.0010128        0.014851       0.0032868       0.0033464
v  Dissip              9.2163e-05        0.030767      0.00045204      0.00039076
v  TurbVisc               0.16486          11.343          4.7137           5.275
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              496:        0.95729E-01

===============================================================


 INSTANT    0.497000000E+03   TIME STEP NUMBER             497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999928E+04
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 :  0.23781E+00 0.12297E+01
   Friction velocity        uet   :  0.14233E-01 0.72575E-01
   Friction velocity        uk    :  0.17431E-01 0.38717E-01
   Dimensionless distance   yplus :  0.42772E+03 0.95379E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64793E+01      58   0.17584E-02   0.21249E-01 
c  VelocityX    0.46300E+04      12   0.71093E-02   0.43441E-03 
c  VelocityY    0.46300E+04      12   0.71093E-02   0.25558E-04 
c  VelocityZ    0.46300E+04      12   0.71093E-02   0.46774E-04 
c  TurbEner     0.59811E+01      13   0.12974E-03   0.17299E-08 
c  Dissip       0.15068E+01      16   0.20584E-02   0.46296E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.98           54519           26776           27270
v  Velocity[x]            0.29284          2.0194         0.90808         0.90985
v  Velocity[y]           -0.36689         0.70038      0.00055145      0.00033187
v  Velocity[z]           -0.42049          0.5058      -0.0012497      -0.0013674
v  TurbEner             0.0010151        0.015459        0.003287       0.0033466
v  Dissip               9.212e-05        0.032373      0.00045228      0.00039095
v  TurbVisc               0.16457          11.369          4.7137          5.2749
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              497:        0.96549E-01

===============================================================


 INSTANT    0.498000000E+03   TIME STEP NUMBER             498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000038E+04
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 :  0.23780E+00 0.13248E+01
   Friction velocity        uet   :  0.14232E-01 0.78966E-01
   Friction velocity        uk    :  0.17451E-01 0.38756E-01
   Dimensionless distance   yplus :  0.42872E+03 0.95376E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59250E+01      52   0.12725E-02   0.19434E-01 
c  VelocityX    0.46300E+04      12   0.66846E-02   0.36469E-03 
c  VelocityY    0.46300E+04      12   0.66846E-02   0.27617E-04 
c  VelocityZ    0.46300E+04      12   0.66846E-02   0.56061E-04 
c  TurbEner     0.59793E+01      14   0.13808E-03   0.23792E-08 
c  Dissip       0.14745E+01      16   0.20903E-02   0.64733E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.08           54529           26776           27271
v  Velocity[x]            0.29286          2.0927         0.90805         0.90983
v  Velocity[y]           -0.38282         0.69579      0.00054786      0.00032796
v  Velocity[z]           -0.42291         0.51045      -0.0012469      -0.0013669
v  TurbEner             0.0010113        0.014888       0.0032869       0.0033465
v  Dissip              9.2056e-05        0.031041      0.00045206       0.0003908
v  TurbVisc                0.1651          11.345          4.7135          5.2748
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              498:        0.96015E-01

===============================================================


 INSTANT    0.499000000E+03   TIME STEP NUMBER             499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997745E+04
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 :  0.23761E+00 0.12136E+01
   Friction velocity        uet   :  0.14220E-01 0.72348E-01
   Friction velocity        uk    :  0.17418E-01 0.38717E-01
   Dimensionless distance   yplus :  0.42824E+03 0.95419E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64638E+01      57   0.13218E-02   0.21179E-01 
c  VelocityX    0.46300E+04      13   0.67997E-02   0.36302E-03 
c  VelocityY    0.46300E+04      13   0.67997E-02   0.35809E-04 
c  VelocityZ    0.46300E+04      13   0.67997E-02   0.41320E-04 
c  TurbEner     0.59791E+01      13   0.70644E-04   0.83303E-09 
c  Dissip       0.14757E+01      14   0.57564E-03   0.41980E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.65           54526           26777           27271
v  Velocity[x]            0.29285          2.1416         0.90806         0.90984
v  Velocity[y]            -0.3674         0.70416       0.0005544      0.00033283
v  Velocity[z]           -0.42082         0.50428      -0.0012531       -0.001372
v  TurbEner              0.001014        0.014757       0.0032867       0.0033464
v  Dissip              9.2074e-05        0.030666      0.00045199      0.00039074
v  TurbVisc               0.16471          11.356          4.7134          5.2747
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              499:        0.95851E-01

===============================================================


 INSTANT    0.500000000E+03   TIME STEP NUMBER             500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998193E+04
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 :  0.23755E+00 0.13251E+01
   Friction velocity        uet   :  0.14215E-01 0.78989E-01
   Friction velocity        uk    :  0.17441E-01 0.38737E-01
   Dimensionless distance   yplus :  0.42796E+03 0.95434E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        500, Physical time    0.50000E+03


   ** 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:    0.75454E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65739E+01      62   0.15418E-02   0.21567E-01 
c  VelocityX    0.46300E+04      12   0.63144E-02   0.37441E-03 
c  VelocityY    0.46300E+04      12   0.63144E-02   0.25430E-04 
c  VelocityZ    0.46300E+04      12   0.63144E-02   0.69478E-04 
c  TurbEner     0.59801E+01      13   0.70952E-04   0.93951E-09 
c  Dissip       0.15012E+01      15   0.78548E-03   0.14562E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.44           54527           26778           27272
v  Velocity[x]            0.29281          2.1886         0.90806         0.90983
v  Velocity[y]           -0.38226         0.69192      0.00056332       0.0003436
v  Velocity[z]           -0.42038         0.51189        -0.00123      -0.0013497
v  TurbEner             0.0010142         0.01485       0.0032868       0.0033464
v  Dissip              9.2054e-05        0.030931      0.00045214      0.00039084
v  TurbVisc                0.1646          11.338          4.7133          5.2745
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              500:        0.10793E+00

===============================================================


 INSTANT    0.501000000E+03   TIME STEP NUMBER             501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998150E+04
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 :  0.23776E+00 0.12185E+01
   Friction velocity        uet   :  0.14227E-01 0.72625E-01
   Friction velocity        uk    :  0.17443E-01 0.38776E-01
   Dimensionless distance   yplus :  0.42842E+03 0.95402E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55486E+01      57   0.14517E-02   0.18196E-01 
c  VelocityX    0.46299E+04      12   0.67439E-02   0.33436E-03 
c  VelocityY    0.46299E+04      12   0.67439E-02   0.24989E-04 
c  VelocityZ    0.46299E+04      12   0.67439E-02   0.41720E-04 
c  TurbEner     0.59795E+01      13   0.12167E-03   0.17541E-08 
c  Dissip       0.15135E+01      16   0.20117E-02   0.46477E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.97           54517           26778           27272
v  Velocity[x]            0.29266          2.0196         0.90804         0.90982
v  Velocity[y]           -0.36615         0.70053      0.00055524      0.00033295
v  Velocity[z]           -0.42279         0.50647      -0.0012541      -0.0013729
v  TurbEner             0.0010117        0.015411       0.0032867       0.0033463
v  Dissip              9.2049e-05        0.032486      0.00045226      0.00039093
v  TurbVisc               0.16486          11.343          4.7132          5.2745
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              501:        0.96061E-01

===============================================================


 INSTANT    0.502000000E+03   TIME STEP NUMBER             502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000385E+04
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 :  0.23777E+00 0.13242E+01
   Friction velocity        uet   :  0.14226E-01 0.78923E-01
   Friction velocity        uk    :  0.17422E-01 0.38731E-01
   Dimensionless distance   yplus :  0.42832E+03 0.95457E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59234E+01      53   0.14423E-02   0.19416E-01 
c  VelocityX    0.46300E+04      12   0.73865E-02   0.34622E-03 
c  VelocityY    0.46300E+04      12   0.73865E-02   0.23641E-04 
c  VelocityZ    0.46300E+04      12   0.73865E-02   0.54866E-04 
c  TurbEner     0.59779E+01      14   0.14005E-03   0.19684E-08 
c  Dissip       0.14799E+01      16   0.21802E-02   0.72350E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.46           54520           26778           27272
v  Velocity[x]            0.29297          2.0928         0.90805         0.90983
v  Velocity[y]            -0.3823         0.69408      0.00055316       0.0003324
v  Velocity[z]           -0.42082         0.51102      -0.0012477      -0.0013696
v  TurbEner             0.0010127        0.014822       0.0032862        0.003346
v  Dissip              9.2076e-05        0.031136      0.00045193       0.0003907
v  TurbVisc               0.16474          11.322          4.7131          5.2744
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              502:        0.95792E-01

===============================================================


 INSTANT    0.503000000E+03   TIME STEP NUMBER             503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000073E+04
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 :  0.23788E+00 0.12171E+01
   Friction velocity        uet   :  0.14231E-01 0.72550E-01
   Friction velocity        uk    :  0.17431E-01 0.38785E-01
   Dimensionless distance   yplus :  0.42775E+03 0.95567E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66075E+01      55   0.14540E-02   0.21669E-01 
c  VelocityX    0.46300E+04      13   0.69677E-02   0.42752E-03 
c  VelocityY    0.46300E+04      13   0.69677E-02   0.44896E-04 
c  VelocityZ    0.46300E+04      13   0.69677E-02   0.42284E-04 
c  TurbEner     0.59780E+01      13   0.64087E-04   0.80278E-09 
c  Dissip       0.14825E+01      14   0.54709E-03   0.41621E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.01           54502           26777           27271
v  Velocity[x]            0.29311          2.1434         0.90806         0.90984
v  Velocity[y]            -0.3677         0.70259      0.00055821      0.00033629
v  Velocity[z]           -0.42115         0.50419      -0.0012458      -0.0013614
v  TurbEner             0.0010147         0.01469       0.0032862       0.0033459
v  Dissip              9.2063e-05        0.030805      0.00045185      0.00039064
v  TurbVisc               0.16449          11.318          4.7129          5.2742
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              503:        0.96117E-01

===============================================================


 INSTANT    0.504000000E+03   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001158E+04
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 :  0.23764E+00 0.13238E+01
   Friction velocity        uet   :  0.14216E-01 0.78902E-01
   Friction velocity        uk    :  0.17448E-01 0.38832E-01
   Dimensionless distance   yplus :  0.42873E+03 0.95578E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58159E+01      60   0.11330E-02   0.19062E-01 
c  VelocityX    0.46300E+04      12   0.69773E-02   0.36790E-03 
c  VelocityY    0.46300E+04      12   0.69773E-02   0.21673E-04 
c  VelocityZ    0.46300E+04      12   0.69773E-02   0.34235E-04 
c  TurbEner     0.59785E+01      13   0.80191E-04   0.11846E-08 
c  Dissip       0.15074E+01      15   0.85051E-03   0.16450E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.18           54510           26777           27271
v  Velocity[x]            0.29252          2.1861         0.90806         0.90983
v  Velocity[y]            -0.3824         0.69502      0.00054554      0.00032729
v  Velocity[z]           -0.42079         0.51172      -0.0012542      -0.0013725
v  TurbEner             0.0010102        0.014797       0.0032861       0.0033459
v  Dissip              9.2106e-05        0.031148      0.00045199      0.00039072
v  TurbVisc               0.16505          11.346          4.7129          5.2742
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              504:        0.96819E-01

===============================================================


 INSTANT    0.505000000E+03   TIME STEP NUMBER             505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001884E+04
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 :  0.23798E+00 0.12163E+01
   Friction velocity        uet   :  0.14235E-01 0.72503E-01
   Friction velocity        uk    :  0.17409E-01 0.38769E-01
   Dimensionless distance   yplus :  0.42813E+03 0.95518E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66130E+01      55   0.16676E-02   0.21678E-01 
c  VelocityX    0.46299E+04      12   0.71869E-02   0.39017E-03 
c  VelocityY    0.46299E+04      12   0.71869E-02   0.26189E-04 
c  VelocityZ    0.46299E+04      12   0.71869E-02   0.81691E-04 
c  TurbEner     0.59789E+01      13   0.11072E-03   0.11324E-08 
c  Dissip       0.15204E+01      16   0.17946E-02   0.35190E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.95           54516           26776           27270
v  Velocity[x]            0.29265          2.0244         0.90806         0.90983
v  Velocity[y]           -0.36652         0.70172      0.00056016      0.00033612
v  Velocity[z]           -0.42112         0.50608      -0.0012506      -0.0013674
v  TurbEner             0.0010122         0.01531       0.0032861       0.0033458
v  Dissip              9.2123e-05        0.032543      0.00045216      0.00039084
v  TurbVisc               0.16461          11.328          4.7129          5.2742
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              505:        0.96525E-01

===============================================================


 INSTANT    0.506000000E+03   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001653E+04
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 :  0.23756E+00 0.13257E+01
   Friction velocity        uet   :  0.14208E-01 0.79019E-01
   Friction velocity        uk    :  0.17425E-01 0.38795E-01
   Dimensionless distance   yplus :  0.42777E+03 0.95340E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61937E+01      62   0.15305E-02   0.20314E-01 
c  VelocityX    0.46298E+04      12   0.64643E-02   0.36619E-03 
c  VelocityY    0.46298E+04      12   0.64643E-02   0.26985E-04 
c  VelocityZ    0.46298E+04      12   0.64643E-02   0.57338E-04 
c  TurbEner     0.59777E+01      14   0.13808E-03   0.23369E-08 
c  Dissip       0.14830E+01      16   0.22406E-02   0.73558E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.04           54515           26777           27271
v  Velocity[x]            0.29321          2.0975         0.90805         0.90983
v  Velocity[y]           -0.38227         0.69317      0.00056437      0.00034549
v  Velocity[z]           -0.41981         0.51105      -0.0012437      -0.0013635
v  TurbEner             0.0010117        0.014721       0.0032861       0.0033458
v  Dissip              9.2104e-05        0.031125       0.0004519      0.00039066
v  TurbVisc               0.16454          11.335          4.7128          5.2741
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              506:        0.97830E-01

===============================================================


 INSTANT    0.507000000E+03   TIME STEP NUMBER             507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997909E+04
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 :  0.23728E+00 0.12162E+01
   Friction velocity        uet   :  0.14192E-01 0.72493E-01
   Friction velocity        uk    :  0.17422E-01 0.38831E-01
   Dimensionless distance   yplus :  0.42819E+03 0.95238E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60272E+01      54   0.12870E-02   0.19756E-01 
c  VelocityX    0.46300E+04      13   0.71728E-02   0.33501E-03 
c  VelocityY    0.46300E+04      13   0.71728E-02   0.34017E-04 
c  VelocityZ    0.46300E+04      13   0.71728E-02   0.38400E-04 
c  TurbEner     0.59771E+01      13   0.69582E-04   0.96086E-09 
c  Dissip       0.14821E+01      14   0.66571E-03   0.51173E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.91           54514           26777           27271
v  Velocity[x]            0.29265          2.1473         0.90806         0.90984
v  Velocity[y]           -0.36695         0.70096      0.00055713      0.00033361
v  Velocity[z]           -0.42064         0.50473      -0.0012454      -0.0013651
v  TurbEner             0.0010084        0.014576       0.0032858       0.0033456
v  Dissip              9.2085e-05        0.030665      0.00045178      0.00039057
v  TurbVisc               0.16483          11.372          4.7128          5.2741
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              507:        0.97299E-01

===============================================================


 INSTANT    0.508000000E+03   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001426E+04
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 :  0.23795E+00 0.13235E+01
   Friction velocity        uet   :  0.14231E-01 0.78891E-01
   Friction velocity        uk    :  0.17393E-01 0.38851E-01
   Dimensionless distance   yplus :  0.42788E+03 0.95187E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58679E+01      52   0.13310E-02   0.19237E-01 
c  VelocityX    0.46300E+04      12   0.71906E-02   0.31323E-03 
c  VelocityY    0.46300E+04      12   0.71906E-02   0.24905E-04 
c  VelocityZ    0.46300E+04      12   0.71906E-02   0.33290E-04 
c  TurbEner     0.59778E+01      12   0.68947E-04   0.66436E-09 
c  Dissip       0.14998E+01      15   0.77178E-03   0.13019E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.22           54515           26777           27271
v  Velocity[x]            0.29264           2.187         0.90805         0.90984
v  Velocity[y]           -0.38236         0.69341       0.0005559      0.00033568
v  Velocity[z]           -0.42165         0.51181      -0.0012423      -0.0013658
v  TurbEner             0.0010088        0.014696       0.0032857       0.0033455
v  Dissip               9.209e-05        0.030968      0.00045184       0.0003906
v  TurbVisc               0.16459          11.352          4.7127           5.274
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              508:        0.95635E-01

===============================================================


 INSTANT    0.509000000E+03   TIME STEP NUMBER             509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000164E+04
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 :  0.23787E+00 0.12273E+01
   Friction velocity        uet   :  0.14226E-01 0.72465E-01
   Friction velocity        uk    :  0.17396E-01 0.38824E-01
   Dimensionless distance   yplus :  0.42707E+03 0.95113E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57493E+01      55   0.14512E-02   0.18848E-01 
c  VelocityX    0.46299E+04      12   0.70810E-02   0.40739E-03 
c  VelocityY    0.46299E+04      12   0.70810E-02   0.26556E-04 
c  VelocityZ    0.46299E+04      12   0.70810E-02   0.44459E-04 
c  TurbEner     0.59783E+01      13   0.12367E-03   0.14606E-08 
c  Dissip       0.15188E+01      16   0.21177E-02   0.48402E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.52           54497           26777           27271
v  Velocity[x]            0.29294          2.0225         0.90806         0.90983
v  Velocity[y]           -0.36686         0.70102      0.00055786      0.00033559
v  Velocity[z]           -0.42007          0.5057      -0.0012434      -0.0013615
v  TurbEner             0.0010109        0.015295       0.0032857       0.0033455
v  Dissip              9.2091e-05        0.032611      0.00045203      0.00039075
v  TurbVisc               0.16433          11.355          4.7126           5.274
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              509:        0.96186E-01

===============================================================


 INSTANT    0.510000000E+03   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999682E+04
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 :  0.23803E+00 0.13248E+01
   Friction velocity        uet   :  0.14236E-01 0.78970E-01
   Friction velocity        uk    :  0.17414E-01 0.38784E-01
   Dimensionless distance   yplus :  0.42797E+03 0.95155E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62008E+01      61   0.13381E-02   0.20326E-01 
c  VelocityX    0.46299E+04      12   0.67524E-02   0.38679E-03 
c  VelocityY    0.46299E+04      12   0.67524E-02   0.25748E-04 
c  VelocityZ    0.46299E+04      12   0.67524E-02   0.94444E-04 
c  TurbEner     0.59766E+01      13   0.13610E-03   0.19773E-08 
c  Dissip       0.14866E+01      16   0.21699E-02   0.66761E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.49           54515           26776           27271
v  Velocity[x]            0.29281          2.0998         0.90805         0.90983
v  Velocity[y]            -0.3828         0.69491      0.00055663      0.00033605
v  Velocity[z]           -0.42209         0.51052      -0.0012416       -0.001363
v  TurbEner             0.0010069        0.014724       0.0032855       0.0033454
v  Dissip              9.2122e-05        0.031219      0.00045182      0.00039061
v  TurbVisc               0.16492          11.314          4.7125          5.2739
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              510:        0.96761E-01

===============================================================


 INSTANT    0.511000000E+03   TIME STEP NUMBER             511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001625E+04
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 :  0.23782E+00 0.12148E+01
   Friction velocity        uet   :  0.14225E-01 0.72325E-01
   Friction velocity        uk    :  0.17380E-01 0.38674E-01
   Dimensionless distance   yplus :  0.42743E+03 0.95213E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64601E+01      56   0.14219E-02   0.21177E-01 
c  VelocityX    0.46300E+04      13   0.69608E-02   0.41320E-03 
c  VelocityY    0.46300E+04      13   0.69608E-02   0.26946E-04 
c  VelocityZ    0.46300E+04      13   0.69608E-02   0.43726E-04 
c  TurbEner     0.59767E+01      12   0.62856E-04   0.64657E-09 
c  Dissip       0.14857E+01      14   0.60131E-03   0.47033E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.34           54513           26776           27270
v  Velocity[x]            0.29281          2.1493         0.90807         0.90985
v  Velocity[y]           -0.36731         0.70249      0.00055395      0.00032815
v  Velocity[z]           -0.42311         0.50436      -0.0012506      -0.0013708
v  TurbEner             0.0010099        0.014604       0.0032854       0.0033453
v  Dissip              9.2103e-05        0.030848      0.00045177      0.00039057
v  TurbVisc               0.16461          11.307          4.7125          5.2739
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              511:        0.96152E-01

===============================================================


 INSTANT    0.512000000E+03   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002234E+04
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 :  0.23759E+00 0.13254E+01
   Friction velocity        uet   :  0.14211E-01 0.79010E-01
   Friction velocity        uk    :  0.17406E-01 0.38680E-01
   Dimensionless distance   yplus :  0.42717E+03 0.95199E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68396E+01      55   0.14937E-02   0.22417E-01 
c  VelocityX    0.46299E+04      12   0.71831E-02   0.38114E-03 
c  VelocityY    0.46299E+04      12   0.71831E-02   0.30614E-04 
c  VelocityZ    0.46299E+04      12   0.71831E-02   0.39981E-04 
c  TurbEner     0.59776E+01      13   0.77233E-04   0.10394E-08 
c  Dissip       0.15042E+01      14   0.62877E-03   0.93617E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.75           54510           26776           27270
v  Velocity[x]            0.29298          2.1872         0.90806         0.90984
v  Velocity[y]            -0.3822         0.69194      0.00056368      0.00034173
v  Velocity[z]           -0.41948         0.51191      -0.0012409      -0.0013594
v  TurbEner             0.0010111        0.014699       0.0032855       0.0033454
v  Dissip               9.209e-05        0.031042      0.00045189      0.00039066
v  TurbVisc               0.16456          11.332          4.7125          5.2739
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              512:        0.95383E-01

===============================================================


 INSTANT    0.513000000E+03   TIME STEP NUMBER             513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001243E+04
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 :  0.23767E+00 0.12173E+01
   Friction velocity        uet   :  0.14217E-01 0.72563E-01
   Friction velocity        uk    :  0.17417E-01 0.38731E-01
   Dimensionless distance   yplus :  0.42785E+03 0.95259E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67074E+01      64   0.13915E-02   0.21998E-01 
c  VelocityX    0.46300E+04      12   0.75667E-02   0.39979E-03 
c  VelocityY    0.46300E+04      12   0.75667E-02   0.48511E-04 
c  VelocityZ    0.46300E+04      12   0.75667E-02   0.32851E-04 
c  TurbEner     0.59776E+01      13   0.11784E-03   0.15695E-08 
c  Dissip       0.15152E+01      16   0.18440E-02   0.36729E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.2           54503           26775           27269
v  Velocity[x]            0.29274          2.0144         0.90808         0.90985
v  Velocity[y]           -0.36603             0.7      0.00055615      0.00033313
v  Velocity[z]           -0.42134          0.5066      -0.0012593       -0.001375
v  TurbEner             0.0010089        0.015268       0.0032855       0.0033453
v  Dissip              9.2049e-05        0.032466      0.00045198      0.00039073
v  TurbVisc               0.16496          11.319          4.7126          5.2739
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              513:        0.97849E-01

===============================================================


 INSTANT    0.514000000E+03   TIME STEP NUMBER             514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000835E+04
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 :  0.23778E+00 0.13237E+01
   Friction velocity        uet   :  0.14225E-01 0.78903E-01
   Friction velocity        uk    :  0.17397E-01 0.38764E-01
   Dimensionless distance   yplus :  0.42777E+03 0.95306E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68904E+01      59   0.14669E-02   0.22569E-01 
c  VelocityX    0.46299E+04      12   0.78727E-02   0.43138E-03 
c  VelocityY    0.46299E+04      12   0.78727E-02   0.23479E-04 
c  VelocityZ    0.46299E+04      12   0.78727E-02   0.54771E-04 
c  TurbEner     0.59766E+01      14   0.13181E-03   0.21640E-08 
c  Dissip       0.14771E+01      16   0.22174E-02   0.71967E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.65           54512           26775           27269
v  Velocity[x]            0.29274           2.093         0.90807         0.90985
v  Velocity[y]           -0.38222         0.69359      0.00055013      0.00033038
v  Velocity[z]           -0.41998         0.51103       -0.001252       -0.001373
v  TurbEner             0.0010101        0.014718       0.0032853       0.0033452
v  Dissip              9.2039e-05        0.031083      0.00045167      0.00039051
v  TurbVisc               0.16479          11.326          4.7125          5.2739
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              514:        0.97050E-01

===============================================================


 INSTANT    0.515000000E+03   TIME STEP NUMBER             515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999285E+04
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 :  0.23798E+00 0.12164E+01
   Friction velocity        uet   :  0.14238E-01 0.72475E-01
   Friction velocity        uk    :  0.17407E-01 0.38772E-01
   Dimensionless distance   yplus :  0.42715E+03 0.95309E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65634E+01      54   0.14595E-02   0.21518E-01 
c  VelocityX    0.46300E+04      13   0.67270E-02   0.45930E-03 
c  VelocityY    0.46300E+04      13   0.67270E-02   0.34511E-04 
c  VelocityZ    0.46300E+04      13   0.67270E-02   0.53690E-04 
c  TurbEner     0.59771E+01      13   0.84693E-04   0.14135E-08 
c  Dissip       0.14813E+01      14   0.53778E-03   0.39472E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.41           54495           26775           27270
v  Velocity[x]            0.29315          2.1442         0.90809         0.90986
v  Velocity[y]           -0.36768         0.70176      0.00055828      0.00033741
v  Velocity[z]           -0.42075         0.50416      -0.0012499      -0.0013672
v  TurbEner             0.0010121        0.014611       0.0032855       0.0033453
v  Dissip               9.202e-05        0.030744      0.00045163      0.00039048
v  TurbVisc               0.16446          11.365          4.7125          5.2738
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              515:        0.95982E-01

===============================================================


 INSTANT    0.516000000E+03   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998911E+04
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 :  0.23767E+00 0.13239E+01
   Friction velocity        uet   :  0.14221E-01 0.78916E-01
   Friction velocity        uk    :  0.17425E-01 0.38760E-01
   Dimensionless distance   yplus :  0.42810E+03 0.95335E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63057E+01      54   0.13529E-02   0.20687E-01 
c  VelocityX    0.46300E+04      12   0.70860E-02   0.30501E-03 
c  VelocityY    0.46300E+04      12   0.70860E-02   0.38404E-04 
c  VelocityZ    0.46300E+04      12   0.70860E-02   0.10685E-03 
c  TurbEner     0.59772E+01      13   0.74188E-04   0.11111E-08 
c  Dissip       0.14989E+01      15   0.67738E-03   0.11290E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.66           54514           26776           27270
v  Velocity[x]            0.29265          2.1888         0.90806         0.90983
v  Velocity[y]           -0.38239         0.69407      0.00055559      0.00033682
v  Velocity[z]           -0.42211         0.51179      -0.0012404      -0.0013628
v  TurbEner             0.0010076        0.014687       0.0032855       0.0033453
v  Dissip              9.2014e-05        0.030888      0.00045172      0.00039053
v  TurbVisc               0.16492          11.344          4.7125          5.2738
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              516:        0.95594E-01

===============================================================


 INSTANT    0.517000000E+03   TIME STEP NUMBER             517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998877E+04
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 :  0.23774E+00 0.12165E+01
   Friction velocity        uet   :  0.14226E-01 0.72516E-01
   Friction velocity        uk    :  0.17386E-01 0.38680E-01
   Dimensionless distance   yplus :  0.42752E+03 0.95329E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61794E+01      56   0.15689E-02   0.20249E-01 
c  VelocityX    0.46298E+04      12   0.75869E-02   0.42416E-03 
c  VelocityY    0.46298E+04      12   0.75869E-02   0.26997E-04 
c  VelocityZ    0.46298E+04      12   0.75869E-02   0.43603E-04 
c  TurbEner     0.59776E+01      13   0.12187E-03   0.12481E-08 
c  Dissip       0.15130E+01      16   0.20559E-02   0.45376E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.1           54508           26775           27269
v  Velocity[x]            0.29248           2.025         0.90806         0.90984
v  Velocity[y]           -0.36652          0.7008      0.00055779      0.00033556
v  Velocity[z]           -0.42016         0.50605      -0.0012505       -0.001372
v  TurbEner             0.0010093        0.015281       0.0032855       0.0033453
v  Dissip              9.2039e-05        0.032474      0.00045192      0.00039069
v  TurbVisc               0.16438          11.347          4.7125          5.2737
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              517:        0.94606E-01

===============================================================


 INSTANT    0.518000000E+03   TIME STEP NUMBER             518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002039E+04
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 :  0.23744E+00 0.13255E+01
   Friction velocity        uet   :  0.14209E-01 0.79002E-01
   Friction velocity        uk    :  0.17401E-01 0.38745E-01
   Dimensionless distance   yplus :  0.42709E+03 0.95363E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63799E+01      58   0.16224E-02   0.20912E-01 
c  VelocityX    0.46299E+04      12   0.62878E-02   0.42352E-03 
c  VelocityY    0.46299E+04      12   0.62878E-02   0.29284E-04 
c  VelocityZ    0.46299E+04      12   0.62878E-02   0.52992E-04 
c  TurbEner     0.59764E+01      14   0.13722E-03   0.21444E-08 
c  Dissip       0.14804E+01      16   0.21021E-02   0.64304E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.26           54505           26775           27270
v  Velocity[x]            0.29327          2.0941         0.90805         0.90983
v  Velocity[y]           -0.38217         0.69442      0.00056235      0.00034177
v  Velocity[z]           -0.41987         0.51112      -0.0012281      -0.0013486
v  TurbEner             0.0010086         0.01473       0.0032853       0.0033452
v  Dissip              9.2048e-05         0.03115      0.00045167      0.00039052
v  TurbVisc                0.1642          11.321          4.7124          5.2736
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              518:        0.96105E-01

===============================================================


 INSTANT    0.519000000E+03   TIME STEP NUMBER             519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999102E+04
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 :  0.23775E+00 0.12133E+01
   Friction velocity        uet   :  0.14228E-01 0.72318E-01
   Friction velocity        uk    :  0.17395E-01 0.38804E-01
   Dimensionless distance   yplus :  0.42739E+03 0.95332E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53929E+01      53   0.11728E-02   0.17685E-01 
c  VelocityX    0.46300E+04      13   0.65961E-02   0.29519E-03 
c  VelocityY    0.46300E+04      13   0.65961E-02   0.25063E-04 
c  VelocityZ    0.46300E+04      13   0.65961E-02   0.51151E-04 
c  TurbEner     0.59761E+01      13   0.79966E-04   0.94072E-09 
c  Dissip       0.14807E+01      14   0.58393E-03   0.44991E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.03           54499           26775           27270
v  Velocity[x]            0.29273          2.1442         0.90806         0.90984
v  Velocity[y]           -0.36687         0.70288      0.00055164       0.0003284
v  Velocity[z]           -0.42241          0.5048      -0.0012499      -0.0013695
v  TurbEner             0.0010052        0.014605       0.0032852       0.0033451
v  Dissip              9.2076e-05        0.030781      0.00045157      0.00039045
v  TurbVisc               0.16434           11.32          4.7123          5.2736
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              519:        0.95847E-01

===============================================================


 INSTANT    0.520000000E+03   TIME STEP NUMBER             520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000275E+04
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 :  0.23775E+00 0.13246E+01
   Friction velocity        uet   :  0.14228E-01 0.78954E-01
   Friction velocity        uk    :  0.17365E-01 0.38780E-01
   Dimensionless distance   yplus :  0.42708E+03 0.95279E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.76330E+01      61   0.15307E-02   0.25019E-01 
c  VelocityX    0.46299E+04      12   0.69968E-02   0.32123E-03 
c  VelocityY    0.46299E+04      12   0.69968E-02   0.46341E-04 
c  VelocityZ    0.46299E+04      12   0.69968E-02   0.85402E-04 
c  TurbEner     0.59770E+01      13   0.63995E-04   0.77978E-09 
c  Dissip       0.15030E+01      15   0.65443E-03   0.10378E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.66           54530           26776           27270
v  Velocity[x]             0.2925          2.1903         0.90805         0.90982
v  Velocity[y]           -0.38236         0.69381      0.00056612      0.00034221
v  Velocity[z]           -0.42156         0.51182      -0.0012341      -0.0013582
v  TurbEner             0.0010053        0.014698       0.0032851       0.0033451
v  Dissip              9.2128e-05        0.030895      0.00045167       0.0003905
v  TurbVisc                 0.164          11.359          4.7123          5.2736
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              520:        0.97435E-01

===============================================================


 INSTANT    0.521000000E+03   TIME STEP NUMBER             521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999615E+04
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 :  0.23789E+00 0.12158E+01
   Friction velocity        uet   :  0.14237E-01 0.72469E-01
   Friction velocity        uk    :  0.17366E-01 0.38772E-01
   Dimensionless distance   yplus :  0.42634E+03 0.95330E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70347E+01      61   0.14621E-02   0.23067E-01 
c  VelocityX    0.46298E+04      12   0.68689E-02   0.39035E-03 
c  VelocityY    0.46298E+04      12   0.68689E-02   0.68728E-04 
c  VelocityZ    0.46298E+04      12   0.68689E-02   0.49586E-04 
c  TurbEner     0.59773E+01      13   0.13528E-03   0.19132E-08 
c  Dissip       0.15066E+01      16   0.19204E-02   0.40255E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.2           54533           26776           27270
v  Velocity[x]            0.29312          2.0091         0.90806         0.90983
v  Velocity[y]           -0.36684         0.70026      0.00054832      0.00032298
v  Velocity[z]           -0.42068         0.50585      -0.0012534      -0.0013751
v  TurbEner             0.0010068        0.015365       0.0032852       0.0033452
v  Dissip              9.2141e-05        0.032368      0.00045182      0.00039062
v  TurbVisc               0.16374          11.347          4.7123          5.2736
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              521:        0.97389E-01

===============================================================


 INSTANT    0.522000000E+03   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998397E+04
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 :  0.23773E+00 0.13253E+01
   Friction velocity        uet   :  0.14228E-01 0.78998E-01
   Friction velocity        uk    :  0.17379E-01 0.38705E-01
   Dimensionless distance   yplus :  0.42718E+03 0.95349E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65480E+01      56   0.12749E-02   0.21463E-01 
c  VelocityX    0.46299E+04      12   0.67333E-02   0.37493E-03 
c  VelocityY    0.46299E+04      12   0.67333E-02   0.36684E-04 
c  VelocityZ    0.46299E+04      12   0.67333E-02   0.29502E-04 
c  TurbEner     0.59770E+01      14   0.13115E-03   0.17983E-08 
c  Dissip       0.14743E+01      16   0.22495E-02   0.69566E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.9           54545           26776           27271
v  Velocity[x]            0.29293          2.1023         0.90806         0.90984
v  Velocity[y]           -0.38278         0.69224      0.00054274      0.00032122
v  Velocity[z]           -0.42301         0.51046       -0.001246       -0.001368
v  TurbEner             0.0010025        0.014774       0.0032852       0.0033451
v  Dissip               9.215e-05        0.030882      0.00045158      0.00039045
v  TurbVisc               0.16424           11.33          4.7124          5.2736
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              522:        0.96920E-01

===============================================================


 INSTANT    0.523000000E+03   TIME STEP NUMBER             523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998853E+04
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 :  0.23754E+00 0.12152E+01
   Friction velocity        uet   :  0.14218E-01 0.72439E-01
   Friction velocity        uk    :  0.17342E-01 0.38694E-01
   Dimensionless distance   yplus :  0.42658E+03 0.95285E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66450E+01      54   0.14750E-02   0.21780E-01 
c  VelocityX    0.46299E+04      12   0.73653E-02   0.35289E-03 
c  VelocityY    0.46299E+04      12   0.73653E-02   0.34872E-04 
c  VelocityZ    0.46299E+04      12   0.73653E-02   0.42568E-04 
c  TurbEner     0.59779E+01      13   0.72880E-04   0.84594E-09 
c  Dissip       0.14793E+01      14   0.32052E-03   0.22967E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.6           54537           26776           27270
v  Velocity[x]            0.29263          2.1426         0.90808         0.90985
v  Velocity[y]           -0.36732         0.70059      0.00054522      0.00032369
v  Velocity[z]           -0.41977         0.50429      -0.0012507      -0.0013733
v  TurbEner             0.0010051        0.014779       0.0032854       0.0033454
v  Dissip              9.2161e-05        0.030742      0.00045159      0.00039047
v  TurbVisc               0.16379          11.364          4.7124          5.2737
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              523:        0.96339E-01

===============================================================


 INSTANT    0.524000000E+03   TIME STEP NUMBER             524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999540E+04
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 :  0.23748E+00 0.13226E+01
   Friction velocity        uet   :  0.14214E-01 0.78840E-01
   Friction velocity        uk    :  0.17365E-01 0.38771E-01
   Dimensionless distance   yplus :  0.42628E+03 0.95299E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60192E+01      60   0.15200E-02   0.19727E-01 
c  VelocityX    0.46299E+04      12   0.75639E-02   0.33902E-03 
c  VelocityY    0.46299E+04      12   0.75639E-02   0.26265E-04 
c  VelocityZ    0.46299E+04      12   0.75639E-02   0.44948E-04 
c  TurbEner     0.59794E+01      13   0.85603E-04   0.14368E-08 
c  Dissip       0.15007E+01      15   0.80712E-03   0.14296E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.13           54514           26777           27271
v  Velocity[x]            0.29296          2.1788         0.90807         0.90985
v  Velocity[y]           -0.38226         0.69334      0.00054964      0.00032927
v  Velocity[z]           -0.42014         0.51187      -0.0012274      -0.0013511
v  TurbEner             0.0010058        0.014961       0.0032857       0.0033456
v  Dissip              9.2146e-05         0.03113      0.00045181      0.00039062
v  TurbVisc               0.16378          11.346          4.7126          5.2738
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              524:        0.97139E-01

===============================================================


 INSTANT    0.525000000E+03   TIME STEP NUMBER             525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998396E+04
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 :  0.23750E+00 0.12156E+01
   Friction velocity        uet   :  0.14216E-01 0.72468E-01
   Friction velocity        uk    :  0.17371E-01 0.38808E-01
   Dimensionless distance   yplus :  0.42682E+03 0.95384E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63921E+01      65   0.13990E-02   0.20967E-01 
c  VelocityX    0.46299E+04      12   0.66659E-02   0.42604E-03 
c  VelocityY    0.46299E+04      12   0.66659E-02   0.29250E-04 
c  VelocityZ    0.46299E+04      12   0.66659E-02   0.51677E-04 
c  TurbEner     0.59798E+01      13   0.81891E-04   0.12105E-08 
c  Dissip       0.15273E+01      15   0.85158E-03   0.15407E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.43           54521           26776           27270
v  Velocity[x]            0.29261           2.201         0.90807         0.90985
v  Velocity[y]            -0.3661          0.7008      0.00055544      0.00033256
v  Velocity[z]           -0.42022         0.50651      -0.0012498      -0.0013704
v  TurbEner             0.0010032        0.015171       0.0032859       0.0033457
v  Dissip               9.213e-05         0.03159      0.00045203      0.00039077
v  TurbVisc               0.16412          11.346          4.7126          5.2739
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              525:        0.99049E-01

===============================================================


 INSTANT    0.526000000E+03   TIME STEP NUMBER             526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001134E+04
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 :  0.23806E+00 0.13244E+01
   Friction velocity        uet   :  0.14250E-01 0.78947E-01
   Friction velocity        uk    :  0.17348E-01 0.38800E-01
   Dimensionless distance   yplus :  0.42654E+03 0.95439E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75803E+01      56   0.16042E-02   0.24846E-01 
c  VelocityX    0.46299E+04      12   0.67837E-02   0.41883E-03 
c  VelocityY    0.46299E+04      12   0.67837E-02   0.26643E-04 
c  VelocityZ    0.46299E+04      12   0.67837E-02   0.92296E-04 
c  TurbEner     0.59802E+01      13   0.13189E-03   0.15982E-08 
c  Dissip       0.15452E+01      16   0.20334E-02   0.49550E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.64           54531           26776           27270
v  Velocity[x]            0.29251          2.0429         0.90805         0.90983
v  Velocity[y]           -0.38224         0.69399      0.00056028      0.00033821
v  Velocity[z]           -0.42105         0.51112      -0.0012413      -0.0013664
v  TurbEner              0.001005        0.015764       0.0032859       0.0033457
v  Dissip              9.2141e-05        0.033203       0.0004523      0.00039096
v  TurbVisc               0.16392          11.376          4.7126          5.2739
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              526:        0.96252E-01

===============================================================


 INSTANT    0.527000000E+03   TIME STEP NUMBER             527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001247E+04
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 :  0.23769E+00 0.12137E+01
   Friction velocity        uet   :  0.14228E-01 0.72315E-01
   Friction velocity        uk    :  0.17364E-01 0.38773E-01
   Dimensionless distance   yplus :  0.42601E+03 0.95449E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70178E+01      57   0.13875E-02   0.23007E-01 
c  VelocityX    0.46298E+04      12   0.68350E-02   0.52526E-03 
c  VelocityY    0.46298E+04      12   0.68350E-02   0.47079E-04 
c  VelocityZ    0.46298E+04      12   0.68350E-02   0.57429E-04 
c  TurbEner     0.59782E+01      13   0.10998E-03   0.15896E-08 
c  Dissip       0.14966E+01      16   0.15776E-02   0.61042E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.59           54538           26775           27269
v  Velocity[x]            0.29325          1.7222         0.90803         0.90981
v  Velocity[y]           -0.36761         0.70182      0.00054844      0.00032542
v  Velocity[z]           -0.42222         0.50423      -0.0012556      -0.0013755
v  TurbEner             0.0010075        0.015724       0.0032859       0.0033457
v  Dissip              9.2078e-05        0.033233      0.00045209      0.00039085
v  TurbVisc                0.1637           11.35          4.7125          5.2738
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              527:        0.96791E-01

===============================================================


 INSTANT    0.528000000E+03   TIME STEP NUMBER             528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002435E+04
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 :  0.23744E+00 0.13250E+01
   Friction velocity        uet   :  0.14212E-01 0.78985E-01
   Friction velocity        uk    :  0.17385E-01 0.38821E-01
   Dimensionless distance   yplus :  0.42702E+03 0.95418E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57037E+01      58   0.12537E-02   0.18707E-01 
c  VelocityX    0.46298E+04      12   0.64993E-02   0.31245E-03 
c  VelocityY    0.46298E+04      12   0.64993E-02   0.35227E-04 
c  VelocityZ    0.46298E+04      12   0.64993E-02   0.32421E-04 
c  TurbEner     0.59738E+01      15   0.40736E-03   0.89634E-08 
c  Dissip       0.13483E+01      18   0.81167E-02   0.47662E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.49           54549           26776           27270
v  Velocity[x]            0.29267          1.8806         0.90804         0.90982
v  Velocity[y]            -0.3824         0.69138      0.00054951      0.00032765
v  Velocity[z]           -0.42138         0.51172       -0.001251       -0.001373
v  TurbEner             0.0010044        0.013518       0.0032855       0.0033454
v  Dissip              9.2028e-05        0.027585      0.00045138      0.00039031
v  TurbVisc               0.16427          11.344          4.7126          5.2739
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              528:        0.18846E+00

===============================================================


 INSTANT    0.529000000E+03   TIME STEP NUMBER             529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997257E+04
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 :  0.23798E+00 0.12166E+01
   Friction velocity        uet   :  0.14245E-01 0.72518E-01
   Friction velocity        uk    :  0.17358E-01 0.38778E-01
   Dimensionless distance   yplus :  0.42671E+03 0.95447E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55859E+01      56   0.11617E-02   0.18322E-01 
c  VelocityX    0.46299E+04      12   0.70663E-02   0.30958E-03 
c  VelocityY    0.46299E+04      12   0.70663E-02   0.21385E-04 
c  VelocityZ    0.46299E+04      12   0.70663E-02   0.39137E-04 
c  TurbEner     0.59726E+01      13   0.15224E-03   0.21396E-08 
c  Dissip       0.12937E+01      18   0.36469E-02   0.12630E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.49           54554           26776           27271
v  Velocity[x]            0.29253          1.9929         0.90805         0.90983
v  Velocity[y]           -0.36656         0.69966      0.00054451      0.00032242
v  Velocity[z]            -0.4215         0.50611      -0.0012576      -0.0013774
v  TurbEner             0.0010075        0.012813       0.0032853       0.0033453
v  Dissip               9.197e-05        0.025272      0.00045073      0.00038986
v  TurbVisc               0.16401          11.381          4.7126          5.2739
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              529:        0.97668E-01

===============================================================


 INSTANT    0.530000000E+03   TIME STEP NUMBER             530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998459E+04
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 :  0.23751E+00 0.13232E+01
   Friction velocity        uet   :  0.14216E-01 0.78873E-01
   Friction velocity        uk    :  0.17385E-01 0.38792E-01
   Dimensionless distance   yplus :  0.42667E+03 0.95427E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69922E+01      60   0.14829E-02   0.22908E-01 
c  VelocityX    0.46299E+04      12   0.73133E-02   0.41060E-03 
c  VelocityY    0.46299E+04      12   0.73133E-02   0.25261E-04 
c  VelocityZ    0.46299E+04      12   0.73133E-02   0.77043E-04 
c  TurbEner     0.59724E+01      13   0.91894E-04   0.14520E-08 
c  Dissip       0.12632E+01      18   0.22947E-02   0.82490E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.99           54546           26776           27271
v  Velocity[x]            0.29303          2.0755         0.90805         0.90983
v  Velocity[y]           -0.38226         0.69369       0.0005549      0.00033499
v  Velocity[z]           -0.41851         0.51109      -0.0012374      -0.0013586
v  TurbEner             0.0010084        0.012729        0.003285       0.0033451
v  Dissip              9.2017e-05        0.024324      0.00045007      0.00038941
v  TurbVisc               0.16402          11.368          4.7127           5.274
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              530:        0.97895E-01

===============================================================


 INSTANT    0.531000000E+03   TIME STEP NUMBER             531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000067E+04
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 :  0.23752E+00 0.12159E+01
   Friction velocity        uet   :  0.14216E-01 0.72483E-01
   Friction velocity        uk    :  0.17393E-01 0.38825E-01
   Dimensionless distance   yplus :  0.42732E+03 0.95371E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72167E+01      65   0.16412E-02   0.23676E-01 
c  VelocityX    0.46299E+04      13   0.66085E-02   0.38882E-03 
c  VelocityY    0.46299E+04      13   0.66085E-02   0.42527E-04 
c  VelocityZ    0.46299E+04      13   0.66085E-02   0.45691E-04 
c  TurbEner     0.59729E+01      13   0.81133E-04   0.13589E-08 
c  Dissip       0.12495E+01      17   0.10402E-02   0.22317E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.04           54519           26777           27271
v  Velocity[x]            0.29283          2.1164         0.90806         0.90984
v  Velocity[y]           -0.36699         0.70128       0.0005515      0.00033109
v  Velocity[z]           -0.42111         0.50475      -0.0012449      -0.0013623
v  TurbEner             0.0010057        0.012929       0.0032849        0.003345
v  Dissip              9.2005e-05        0.024032      0.00044954      0.00038904
v  TurbVisc               0.16437          11.318          4.7128          5.2741
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              531:        0.98855E-01

===============================================================


 INSTANT    0.532000000E+03   TIME STEP NUMBER             532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999691E+04
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 :  0.23766E+00 0.13241E+01
   Friction velocity        uet   :  0.14224E-01 0.78927E-01
   Friction velocity        uk    :  0.17370E-01 0.38856E-01
   Dimensionless distance   yplus :  0.42718E+03 0.95379E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66807E+01      59   0.12757E-02   0.21898E-01 
c  VelocityX    0.46300E+04      12   0.71811E-02   0.35107E-03 
c  VelocityY    0.46300E+04      12   0.71811E-02   0.45303E-04 
c  VelocityZ    0.46300E+04      12   0.71811E-02   0.28404E-04 
c  TurbEner     0.59734E+01      13   0.84795E-04   0.11949E-08 
c  Dissip       0.12541E+01      16   0.52460E-03   0.64979E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.39           54532           26777           27271
v  Velocity[x]            0.29257          2.1655         0.90804         0.90982
v  Velocity[y]           -0.38242         0.69396      0.00055565      0.00033433
v  Velocity[z]           -0.42162         0.51186       -0.001237      -0.0013613
v  TurbEner              0.001007        0.013268       0.0032849       0.0033451
v  Dissip              9.2012e-05        0.024269      0.00044922      0.00038882
v  TurbVisc               0.16415          11.307          4.7129          5.2742
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              532:        0.97411E-01

===============================================================


 INSTANT    0.533000000E+03   TIME STEP NUMBER             533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999209E+04
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 :  0.23773E+00 0.12164E+01
   Friction velocity        uet   :  0.14227E-01 0.72509E-01
   Friction velocity        uk    :  0.17381E-01 0.38859E-01
   Dimensionless distance   yplus :  0.42659E+03 0.95347E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60362E+01      59   0.13815E-02   0.19794E-01 
c  VelocityX    0.46300E+04      12   0.65988E-02   0.34292E-03 
c  VelocityY    0.46300E+04      12   0.65988E-02   0.34727E-04 
c  VelocityZ    0.46300E+04      12   0.65988E-02   0.41242E-04 
c  TurbEner     0.59741E+01      14   0.14402E-03   0.21763E-08 
c  Dissip       0.12641E+01      16   0.19225E-02   0.35963E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.67           54537           26776           27271
v  Velocity[x]             0.2931          1.9973         0.90804         0.90981
v  Velocity[y]           -0.36691         0.70132      0.00054857      0.00032461
v  Velocity[z]           -0.42061         0.50574      -0.0012506      -0.0013706
v  TurbEner             0.0010092        0.014062        0.003285       0.0033451
v  Dissip              9.1989e-05        0.025677      0.00044906      0.00038872
v  TurbVisc               0.16397          11.333          4.7131          5.2743
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              533:        0.97520E-01

===============================================================


 INSTANT    0.534000000E+03   TIME STEP NUMBER             534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001742E+04
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 :  0.23781E+00 0.13252E+01
   Friction velocity        uet   :  0.14231E-01 0.78986E-01
   Friction velocity        uk    :  0.17400E-01 0.38865E-01
   Dimensionless distance   yplus :  0.42758E+03 0.95331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65642E+01      53   0.14224E-02   0.21527E-01 
c  VelocityX    0.46300E+04      13   0.72048E-02   0.32669E-03 
c  VelocityY    0.46300E+04      13   0.72048E-02   0.35605E-04 
c  VelocityZ    0.46300E+04      13   0.72048E-02   0.10457E-03 
c  TurbEner     0.59739E+01      13   0.80356E-04   0.97146E-09 
c  Dissip       0.12456E+01      16   0.15375E-02   0.35128E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.51           54544           26777           27271
v  Velocity[x]            0.29277          2.0823         0.90804         0.90982
v  Velocity[y]           -0.38285         0.69504      0.00054915      0.00032655
v  Velocity[z]           -0.42132         0.51051      -0.0012409      -0.0013635
v  TurbEner             0.0010054        0.013788       0.0032849       0.0033451
v  Dissip              9.2037e-05        0.024805      0.00044867      0.00038845
v  TurbVisc               0.16457          11.317          4.7133          5.2745
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              534:        0.97181E-01

===============================================================


 INSTANT    0.535000000E+03   TIME STEP NUMBER             535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000242E+04
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 :  0.23786E+00 0.12144E+01
   Friction velocity        uet   :  0.14232E-01 0.72339E-01
   Friction velocity        uk    :  0.17367E-01 0.38769E-01
   Dimensionless distance   yplus :  0.42709E+03 0.95338E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68884E+01      58   0.15624E-02   0.22577E-01 
c  VelocityX    0.46301E+04      13   0.72071E-02   0.44190E-03 
c  VelocityY    0.46301E+04      13   0.72071E-02   0.38568E-04 
c  VelocityZ    0.46301E+04      13   0.72071E-02   0.54341E-04 
c  TurbEner     0.59745E+01      13   0.73050E-04   0.91023E-09 
c  Dissip       0.12538E+01      15   0.44744E-03   0.50547E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.34           54537           26776           27270
v  Velocity[x]            0.29279          2.1336         0.90808         0.90985
v  Velocity[y]           -0.36744         0.70225      0.00054969      0.00032654
v  Velocity[z]           -0.42082         0.50433      -0.0012504      -0.0013699
v  TurbEner             0.0010081        0.013914       0.0032851       0.0033451
v  Dissip               9.211e-05        0.024803      0.00044858      0.00038839
v  TurbVisc               0.16429          11.327          4.7134          5.2747
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              535:        0.10044E+00

===============================================================


 INSTANT    0.536000000E+03   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000995E+04
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 :  0.23771E+00 0.13254E+01
   Friction velocity        uet   :  0.14222E-01 0.79004E-01
   Friction velocity        uk    :  0.17391E-01 0.38788E-01
   Dimensionless distance   yplus :  0.42685E+03 0.95294E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65562E+01      66   0.14761E-02   0.21481E-01 
c  VelocityX    0.46301E+04      12   0.75705E-02   0.43658E-03 
c  VelocityY    0.46301E+04      12   0.75705E-02   0.27820E-04 
c  VelocityZ    0.46301E+04      12   0.75705E-02   0.37199E-04 
c  TurbEner     0.59762E+01      13   0.99164E-04   0.17068E-08 
c  Dissip       0.12778E+01      16   0.10498E-02   0.22181E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.75           54513           26777           27271
v  Velocity[x]            0.29295          2.1726         0.90807         0.90986
v  Velocity[y]           -0.38226         0.69164      0.00055019      0.00033199
v  Velocity[z]           -0.42008         0.51187      -0.0012363      -0.0013558
v  TurbEner             0.0010085        0.014212       0.0032854       0.0033453
v  Dissip              9.2148e-05        0.025302      0.00044871      0.00038848
v  TurbVisc                0.1643          11.365          4.7136          5.2749
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              536:        0.99140E-01

===============================================================


 INSTANT    0.537000000E+03   TIME STEP NUMBER             537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999299E+04
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 :  0.23736E+00 0.12175E+01
   Friction velocity        uet   :  0.14200E-01 0.72569E-01
   Friction velocity        uk    :  0.17394E-01 0.38818E-01
   Dimensionless distance   yplus :  0.42730E+03 0.95331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65596E+01      62   0.14166E-02   0.21526E-01 
c  VelocityX    0.46302E+04      12   0.65277E-02   0.41178E-03 
c  VelocityY    0.46302E+04      12   0.65277E-02   0.39702E-04 
c  VelocityZ    0.46302E+04      12   0.65277E-02   0.35846E-04 
c  TurbEner     0.59764E+01      14   0.13882E-03   0.26811E-08 
c  Dissip       0.12981E+01      17   0.21060E-02   0.53013E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.93           54523           26777           27271
v  Velocity[x]            0.29278          2.0013         0.90806         0.90984
v  Velocity[y]           -0.36612         0.69947      0.00054498      0.00032292
v  Velocity[z]            -0.4219         0.50662      -0.0012606      -0.0013762
v  TurbEner             0.0010066        0.014942       0.0032857       0.0033455
v  Dissip              9.2131e-05         0.02689      0.00044891      0.00038862
v  TurbVisc               0.16466          11.346          4.7139          5.2751
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              537:        0.97993E-01

===============================================================


 INSTANT    0.538000000E+03   TIME STEP NUMBER             538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999852E+04
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 :  0.23784E+00 0.13240E+01
   Friction velocity        uet   :  0.14227E-01 0.78915E-01
   Friction velocity        uk    :  0.17377E-01 0.38857E-01
   Dimensionless distance   yplus :  0.42727E+03 0.95359E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61899E+01      55   0.13199E-02   0.20294E-01 
c  VelocityX    0.46302E+04      12   0.70299E-02   0.32568E-03 
c  VelocityY    0.46302E+04      12   0.70299E-02   0.37073E-04 
c  VelocityZ    0.46302E+04      12   0.70299E-02   0.60216E-04 
c  TurbEner     0.59757E+01      14   0.97707E-04   0.15838E-08 
c  Dissip       0.12855E+01      16   0.12782E-02   0.27944E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.96           54535           26777           27271
v  Velocity[x]            0.29255          2.0819         0.90805         0.90983
v  Velocity[y]           -0.38233         0.69453       0.0005458      0.00032565
v  Velocity[z]           -0.42119         0.51107      -0.0012404      -0.0013599
v  TurbEner              0.001009         0.01456       0.0032857       0.0033454
v  Dissip              9.2147e-05        0.026161      0.00044879      0.00038852
v  TurbVisc               0.16468          11.348          4.7141          5.2752
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              538:        0.97007E-01

===============================================================


 INSTANT    0.539000000E+03   TIME STEP NUMBER             539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998389E+04
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 :  0.23801E+00 0.12126E+01
   Friction velocity        uet   :  0.14236E-01 0.72276E-01
   Friction velocity        uk    :  0.17398E-01 0.38863E-01
   Dimensionless distance   yplus :  0.42689E+03 0.95314E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57803E+01      57   0.12658E-02   0.18947E-01 
c  VelocityX    0.46301E+04      13   0.62934E-02   0.33806E-03 
c  VelocityY    0.46301E+04      13   0.62934E-02   0.24793E-04 
c  VelocityZ    0.46301E+04      13   0.62934E-02   0.40760E-04 
c  TurbEner     0.59767E+01      12   0.70535E-04   0.70944E-09 
c  Dissip       0.13005E+01      15   0.52838E-03   0.72752E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -179.1           54541           26776           27271
v  Velocity[x]            0.29268          2.1333         0.90805         0.90983
v  Velocity[y]           -0.36777         0.70358      0.00054882      0.00032484
v  Velocity[z]           -0.42084         0.50417      -0.0012538      -0.0013723
v  TurbEner             0.0010124        0.014555        0.003286       0.0033456
v  Dissip              9.2088e-05        0.026211       0.0004489      0.00038859
v  TurbVisc               0.16464           11.31          4.7142          5.2753
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              539:        0.97743E-01

===============================================================


 INSTANT    0.540000000E+03   TIME STEP NUMBER             540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002154E+04
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 :  0.23783E+00 0.13249E+01
   Friction velocity        uet   :  0.14224E-01 0.78969E-01
   Friction velocity        uk    :  0.17427E-01 0.38830E-01
   Dimensionless distance   yplus :  0.42812E+03 0.95349E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55247E+01      57   0.12472E-02   0.18121E-01 
c  VelocityX    0.46303E+04      12   0.67200E-02   0.28835E-03 
c  VelocityY    0.46303E+04      12   0.67200E-02   0.33310E-04 
c  VelocityZ    0.46303E+04      12   0.67200E-02   0.83109E-04 
c  TurbEner     0.59781E+01      13   0.77026E-04   0.97011E-09 
c  Dissip       0.13279E+01      16   0.10104E-02   0.22731E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.11           54550           26777           27271
v  Velocity[x]            0.29306          2.1756         0.90806         0.90984
v  Velocity[y]           -0.38252         0.69133      0.00054671      0.00032664
v  Velocity[z]           -0.42274         0.51175      -0.0012408      -0.0013623
v  TurbEner             0.0010099        0.014719       0.0032863       0.0033458
v  Dissip              9.2081e-05        0.026671       0.0004492      0.00038879
v  TurbVisc               0.16545          11.307          4.7145          5.2756
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              540:        0.96339E-01

===============================================================


 INSTANT    0.541000000E+03   TIME STEP NUMBER             541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998259E+04
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 :  0.23766E+00 0.12480E+01
   Friction velocity        uet   :  0.14213E-01 0.72733E-01
   Friction velocity        uk    :  0.17406E-01 0.38734E-01
   Dimensionless distance   yplus :  0.42791E+03 0.95355E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56639E+01      53   0.15225E-02   0.18578E-01 
c  VelocityX    0.46302E+04      12   0.65851E-02   0.33400E-03 
c  VelocityY    0.46302E+04      12   0.65851E-02   0.25519E-04 
c  VelocityZ    0.46302E+04      12   0.65851E-02   0.39544E-04 
c  TurbEner     0.59790E+01      13   0.11986E-03   0.14359E-08 
c  Dissip       0.13517E+01      17   0.21891E-02   0.58990E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.66           54556           26777           27272
v  Velocity[x]            0.29295          2.0146         0.90805         0.90983
v  Velocity[y]           -0.36658         0.70086      0.00054814      0.00032599
v  Velocity[z]           -0.41957         0.50601      -0.0012527      -0.0013723
v  TurbEner             0.0010142        0.015378       0.0032867       0.0033461
v  Dissip              9.2054e-05        0.028366      0.00044964       0.0003891
v  TurbVisc               0.16537          11.332          4.7146          5.2757
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              541:        0.93960E-01

===============================================================


 INSTANT    0.542000000E+03   TIME STEP NUMBER             542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999149E+04
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 :  0.23765E+00 0.13239E+01
   Friction velocity        uet   :  0.14212E-01 0.78908E-01
   Friction velocity        uk    :  0.17443E-01 0.38745E-01
   Dimensionless distance   yplus :  0.42796E+03 0.95344E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62551E+01      61   0.15598E-02   0.20503E-01 
c  VelocityX    0.46302E+04      12   0.74140E-02   0.34611E-03 
c  VelocityY    0.46302E+04      12   0.74140E-02   0.25551E-04 
c  VelocityZ    0.46302E+04      12   0.74140E-02   0.47458E-04 
c  TurbEner     0.59785E+01      14   0.11139E-03   0.17255E-08 
c  Dissip       0.13354E+01      16   0.14228E-02   0.35437E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.46           54547           26778           27272
v  Velocity[x]            0.29286          2.0851         0.90806         0.90985
v  Velocity[y]            -0.3823         0.69493      0.00055022      0.00033108
v  Velocity[z]           -0.42015         0.51106      -0.0012396       -0.001361
v  TurbEner             0.0010168        0.014883       0.0032869       0.0033463
v  Dissip              9.2073e-05        0.027532      0.00044968      0.00038913
v  TurbVisc               0.16557          11.382          4.7148          5.2759
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              542:        0.96593E-01

===============================================================


 INSTANT    0.543000000E+03   TIME STEP NUMBER             543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997676E+04
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 :  0.23762E+00 0.12175E+01
   Friction velocity        uet   :  0.14210E-01 0.72580E-01
   Friction velocity        uk    :  0.17465E-01 0.38803E-01
   Dimensionless distance   yplus :  0.42889E+03 0.95350E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66050E+01      55   0.15173E-02   0.21657E-01 
c  VelocityX    0.46304E+04      13   0.70045E-02   0.46234E-03 
c  VelocityY    0.46304E+04      13   0.70045E-02   0.27641E-04 
c  VelocityZ    0.46304E+04      13   0.70045E-02   0.54812E-04 
c  TurbEner     0.59791E+01      13   0.67024E-04   0.10647E-08 
c  Dissip       0.13482E+01      15   0.43537E-03   0.54158E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.13           54520           26778           27273
v  Velocity[x]            0.29268          2.1361         0.90808         0.90986
v  Velocity[y]           -0.36702         0.70314      0.00054962      0.00032889
v  Velocity[z]           -0.42155         0.50471      -0.0012504      -0.0013672
v  TurbEner             0.0010165        0.014806       0.0032872       0.0033466
v  Dissip              9.2056e-05        0.027508      0.00044987      0.00038926
v  TurbVisc               0.16624          11.369           4.715           5.276
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              543:        0.95988E-01

===============================================================


 INSTANT    0.544000000E+03   TIME STEP NUMBER             544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998696E+04
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 :  0.23771E+00 0.13235E+01
   Friction velocity        uet   :  0.14215E-01 0.78884E-01
   Friction velocity        uk    :  0.17463E-01 0.38827E-01
   Dimensionless distance   yplus :  0.42917E+03 0.95343E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64748E+01      56   0.13200E-02   0.21230E-01 
c  VelocityX    0.46304E+04      12   0.67946E-02   0.37535E-03 
c  VelocityY    0.46304E+04      12   0.67946E-02   0.62755E-04 
c  VelocityZ    0.46304E+04      12   0.67946E-02   0.10597E-03 
c  TurbEner     0.59797E+01      13   0.73460E-04   0.11535E-08 
c  Dissip       0.13773E+01      16   0.96985E-03   0.21376E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.39           54528           26779           27273
v  Velocity[x]            0.29299          2.1776         0.90806         0.90984
v  Velocity[y]           -0.38244         0.69574      0.00055294      0.00033406
v  Velocity[z]           -0.42083         0.51177      -0.0012328      -0.0013544
v  TurbEner             0.0010205        0.014953       0.0032875       0.0033467
v  Dissip              9.2077e-05        0.027977      0.00045021      0.00038947
v  TurbVisc               0.16646          11.372          4.7152          5.2762
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              544:        0.95610E-01

===============================================================


 INSTANT    0.545000000E+03   TIME STEP NUMBER             545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997915E+04
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 :  0.23798E+00 0.12228E+01
   Friction velocity        uet   :  0.14231E-01 0.72545E-01
   Friction velocity        uk    :  0.17497E-01 0.38794E-01
   Dimensionless distance   yplus :  0.42904E+03 0.95307E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57167E+01      58   0.13465E-02   0.18750E-01 
c  VelocityX    0.46303E+04      12   0.67876E-02   0.39676E-03 
c  VelocityY    0.46303E+04      12   0.67876E-02   0.24284E-04 
c  VelocityZ    0.46303E+04      12   0.67876E-02   0.46651E-04 
c  TurbEner     0.59803E+01      14   0.13049E-03   0.17664E-08 
c  Dissip       0.14010E+01      17   0.22114E-02   0.62458E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.49           54528           26779           27273
v  Velocity[x]            0.29312          2.0105         0.90805         0.90983
v  Velocity[y]            -0.3669         0.70138      0.00055255      0.00033157
v  Velocity[z]            -0.4213         0.50576      -0.0012509      -0.0013725
v  TurbEner              0.001026        0.015608       0.0032878       0.0033469
v  Dissip              9.2076e-05        0.029693      0.00045064      0.00038977
v  TurbVisc               0.16662          11.344          4.7153          5.2763
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              545:        0.95882E-01

===============================================================


 INSTANT    0.546000000E+03   TIME STEP NUMBER             546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001424E+04
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 :  0.23773E+00 0.13263E+01
   Friction velocity        uet   :  0.14217E-01 0.79052E-01
   Friction velocity        uk    :  0.17545E-01 0.38771E-01
   Dimensionless distance   yplus :  0.43064E+03 0.95295E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58916E+01      67   0.14378E-02   0.19339E-01 
c  VelocityX    0.46304E+04      12   0.64950E-02   0.33422E-03 
c  VelocityY    0.46304E+04      12   0.64950E-02   0.27647E-04 
c  VelocityZ    0.46304E+04      12   0.64950E-02   0.47421E-04 
c  TurbEner     0.59788E+01      13   0.12213E-03   0.18371E-08 
c  Dissip       0.13785E+01      16   0.16567E-02   0.45993E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.93           54510           26780           27274
v  Velocity[x]            0.29247          2.0862         0.90806         0.90984
v  Velocity[y]           -0.38291         0.69252      0.00055112      0.00033331
v  Velocity[z]           -0.42229         0.51049      -0.0012377      -0.0013591
v  TurbEner             0.0010258        0.015051       0.0032878       0.0033469
v  Dissip              9.2085e-05        0.028676      0.00045063      0.00038976
v  TurbVisc               0.16769          11.336          4.7154          5.2764
v  total_pressure           83077      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              546:        0.98585E-01

===============================================================


 INSTANT    0.547000000E+03   TIME STEP NUMBER             547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999999E+04
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 :  0.23764E+00 0.12164E+01
   Friction velocity        uet   :  0.14212E-01 0.72504E-01
   Friction velocity        uk    :  0.17542E-01 0.38607E-01
   Dimensionless distance   yplus :  0.43084E+03 0.95239E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58180E+01      60   0.12211E-02   0.19077E-01 
c  VelocityX    0.46304E+04      13   0.70481E-02   0.33190E-03 
c  VelocityY    0.46304E+04      13   0.70481E-02   0.23747E-04 
c  VelocityZ    0.46304E+04      13   0.70481E-02   0.51190E-04 
c  TurbEner     0.59780E+01      13   0.64000E-04   0.10072E-08 
c  Dissip       0.13900E+01      14   0.41310E-03   0.46953E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.93           54520           26779           27273
v  Velocity[x]            0.29262          2.1368         0.90806         0.90984
v  Velocity[y]           -0.36743         0.70027      0.00054824      0.00032557
v  Velocity[z]           -0.41993         0.50429      -0.0012527      -0.0013734
v  TurbEner             0.0010325        0.014954       0.0032877       0.0033468
v  Dissip              9.2058e-05        0.028597      0.00045077      0.00038984
v  TurbVisc               0.16788          11.366          4.7154          5.2764
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              547:        0.97352E-01

===============================================================


 INSTANT    0.548000000E+03   TIME STEP NUMBER             548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002162E+04
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 :  0.23763E+00 0.13227E+01
   Friction velocity        uet   :  0.14211E-01 0.78839E-01
   Friction velocity        uk    :  0.17600E-01 0.38682E-01
   Dimensionless distance   yplus :  0.43132E+03 0.95229E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59327E+01      63   0.13721E-02   0.19444E-01 
c  VelocityX    0.46304E+04      12   0.67837E-02   0.30866E-03 
c  VelocityY    0.46304E+04      12   0.67837E-02   0.36764E-04 
c  VelocityZ    0.46304E+04      12   0.67837E-02   0.90578E-04 
c  TurbEner     0.59788E+01      13   0.64352E-04   0.70445E-09 
c  Dissip       0.14168E+01      15   0.88582E-03   0.17655E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.28           54535           26778           27272
v  Velocity[x]            0.29324          2.1781         0.90806         0.90984
v  Velocity[y]           -0.38224         0.69309      0.00054996      0.00032954
v  Velocity[z]           -0.42085         0.51192      -0.0012402      -0.0013624
v  TurbEner              0.001037        0.015061       0.0032877       0.0033467
v  Dissip              9.2078e-05        0.029016      0.00045102      0.00038998
v  TurbVisc               0.16835           11.35          4.7154          5.2764
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              548:        0.90330E-01

===============================================================


 INSTANT    0.549000000E+03   TIME STEP NUMBER             549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001052E+04
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 :  0.23782E+00 0.12156E+01
   Friction velocity        uet   :  0.14223E-01 0.72462E-01
   Friction velocity        uk    :  0.17638E-01 0.38749E-01
   Dimensionless distance   yplus :  0.43265E+03 0.95207E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56104E+01      54   0.13855E-02   0.18408E-01 
c  VelocityX    0.46303E+04      12   0.66846E-02   0.31736E-03 
c  VelocityY    0.46303E+04      12   0.66846E-02   0.28846E-04 
c  VelocityZ    0.46303E+04      12   0.66846E-02   0.42193E-04 
c  TurbEner     0.59795E+01      13   0.12078E-03   0.14300E-08 
c  Dissip       0.14400E+01      16   0.22020E-02   0.58924E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.12           54544           26778           27272
v  Velocity[x]            0.29264          2.0138         0.90805         0.90982
v  Velocity[y]           -0.36612         0.70035      0.00055024      0.00032614
v  Velocity[z]           -0.42035         0.50649      -0.0012598      -0.0013804
v  TurbEner             0.0010383        0.015679       0.0032879       0.0033468
v  Dissip              9.2072e-05         0.03075      0.00045135      0.00039021
v  TurbVisc                0.1692          11.334          4.7154          5.2765
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              549:        0.88862E-01

===============================================================


 INSTANT    0.550000000E+03   TIME STEP NUMBER             550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000752E+04
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 :  0.23819E+00 0.13248E+01
   Friction velocity        uet   :  0.14245E-01 0.78967E-01
   Friction velocity        uk    :  0.17649E-01 0.38769E-01
   Dimensionless distance   yplus :  0.43331E+03 0.95187E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59710E+01      54   0.13284E-02   0.19573E-01 
c  VelocityX    0.46303E+04      12   0.69694E-02   0.33672E-03 
c  VelocityY    0.46303E+04      12   0.69694E-02   0.22496E-04 
c  VelocityZ    0.46303E+04      12   0.69694E-02   0.52752E-04 
c  TurbEner     0.59781E+01      14   0.13416E-03   0.20083E-08 
c  Dissip       0.14159E+01      16   0.17666E-02   0.50319E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.06           54551           26778           27272
v  Velocity[x]            0.29269          2.0845         0.90806         0.90984
v  Velocity[y]           -0.38228         0.69396      0.00054772      0.00032794
v  Velocity[z]           -0.42123         0.51109      -0.0012573      -0.0013777
v  TurbEner             0.0010432        0.015082       0.0032878       0.0033466
v  Dissip              9.2045e-05        0.029638      0.00045125      0.00039013
v  TurbVisc               0.16954          11.364          4.7155          5.2765
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              550:        0.89429E-01

===============================================================


 INSTANT    0.551000000E+03   TIME STEP NUMBER             551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999011E+04
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 :  0.23778E+00 0.12140E+01
   Friction velocity        uet   :  0.14221E-01 0.72320E-01
   Friction velocity        uk    :  0.17690E-01 0.38759E-01
   Dimensionless distance   yplus :  0.43348E+03 0.95238E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64881E+01      52   0.14565E-02   0.21263E-01 
c  VelocityX    0.46303E+04      12   0.69303E-02   0.41475E-03 
c  VelocityY    0.46303E+04      12   0.69303E-02   0.27395E-04 
c  VelocityZ    0.46303E+04      12   0.69303E-02   0.41353E-04 
c  TurbEner     0.59787E+01      13   0.68070E-04   0.83158E-09 
c  Dissip       0.14229E+01      14   0.46664E-03   0.37802E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.76           54544           26778           27272
v  Velocity[x]            0.29296          2.1378         0.90808         0.90986
v  Velocity[y]           -0.36767         0.70209      0.00054625      0.00032483
v  Velocity[z]           -0.42153         0.50422      -0.0012598      -0.0013769
v  TurbEner             0.0010486        0.014911        0.003288       0.0033468
v  Dissip              9.2041e-05        0.029404      0.00045136       0.0003902
v  TurbVisc                0.1697          11.345          4.7155          5.2765
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              551:        0.88625E-01

===============================================================


 INSTANT    0.552000000E+03   TIME STEP NUMBER             552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000387E+04
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 :  0.23758E+00 0.13251E+01
   Friction velocity        uet   :  0.14209E-01 0.78988E-01
   Friction velocity        uk    :  0.17737E-01 0.38740E-01
   Dimensionless distance   yplus :  0.43517E+03 0.95258E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66548E+01      60   0.15387E-02   0.21826E-01 
c  VelocityX    0.46303E+04      12   0.74753E-02   0.38215E-03 
c  VelocityY    0.46303E+04      12   0.74753E-02   0.42194E-04 
c  VelocityZ    0.46303E+04      12   0.74753E-02   0.33207E-04 
c  TurbEner     0.59801E+01      13   0.77206E-04   0.13368E-08 
c  Dissip       0.14475E+01      15   0.78861E-03   0.15218E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.09           54524           26778           27272
v  Velocity[x]            0.29274          2.1797         0.90808         0.90985
v  Velocity[y]           -0.38244         0.69205      0.00055087      0.00033269
v  Velocity[z]           -0.42142         0.51169      -0.0012434      -0.0013637
v  TurbEner             0.0010466         0.01498       0.0032883       0.0033471
v  Dissip              9.2034e-05        0.029687       0.0004516      0.00039037
v  TurbVisc               0.17062          11.347          4.7157          5.2767
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              552:        0.89723E-01

===============================================================


 INSTANT    0.553000000E+03   TIME STEP NUMBER             553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998859E+04
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 :  0.23779E+00 0.12167E+01
   Friction velocity        uet   :  0.14221E-01 0.72523E-01
   Friction velocity        uk    :  0.17720E-01 0.38677E-01
   Dimensionless distance   yplus :  0.43516E+03 0.95266E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56687E+01      57   0.14817E-02   0.18595E-01 
c  VelocityX    0.46302E+04      12   0.67937E-02   0.37946E-03 
c  VelocityY    0.46302E+04      12   0.67937E-02   0.45189E-04 
c  VelocityZ    0.46302E+04      12   0.67937E-02   0.84680E-04 
c  TurbEner     0.59801E+01      13   0.11803E-03   0.17320E-08 
c  Dissip       0.14632E+01      16   0.19539E-02   0.45345E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.45           54529           26777           27272
v  Velocity[x]            0.29289          2.0144         0.90805         0.90982
v  Velocity[y]           -0.36658         0.70067      0.00055477       0.0003315
v  Velocity[z]           -0.42098         0.50605      -0.0012576      -0.0013766
v  TurbEner             0.0010507        0.015583       0.0032886       0.0033473
v  Dissip              9.2041e-05        0.031216       0.0004519      0.00039058
v  TurbVisc               0.17045          11.323          4.7158          5.2768
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              553:        0.89581E-01

===============================================================


 INSTANT    0.554000000E+03   TIME STEP NUMBER             554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001473E+04
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 :  0.23775E+00 0.13244E+01
   Friction velocity        uet   :  0.14219E-01 0.78939E-01
   Friction velocity        uk    :  0.17755E-01 0.38766E-01
   Dimensionless distance   yplus :  0.43528E+03 0.95332E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61054E+01      53   0.13740E-02   0.20018E-01 
c  VelocityX    0.46301E+04      12   0.62189E-02   0.33158E-03 
c  VelocityY    0.46301E+04      12   0.62189E-02   0.22850E-04 
c  VelocityZ    0.46301E+04      12   0.62189E-02   0.51176E-04 
c  TurbEner     0.59791E+01      14   0.12633E-03   0.19519E-08 
c  Dissip       0.14371E+01      16   0.18371E-02   0.55201E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.52           54537           26778           27272
v  Velocity[x]            0.29278          2.0857         0.90804         0.90982
v  Velocity[y]           -0.38232         0.69552      0.00054842      0.00032745
v  Velocity[z]           -0.41904           0.511      -0.0012441      -0.0013658
v  TurbEner             0.0010518        0.015052       0.0032885       0.0033472
v  Dissip              9.2011e-05        0.030088      0.00045176      0.00039049
v  TurbVisc               0.17049          11.313          4.7159          5.2769
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              554:        0.89052E-01

===============================================================


 INSTANT    0.555000000E+03   TIME STEP NUMBER             555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999568E+04
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 :  0.23763E+00 0.12138E+01
   Friction velocity        uet   :  0.14213E-01 0.72357E-01
   Friction velocity        uk    :  0.17763E-01 0.38805E-01
   Dimensionless distance   yplus :  0.43602E+03 0.95371E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53354E+01      57   0.11349E-02   0.17500E-01 
c  VelocityX    0.46303E+04      13   0.61301E-02   0.28816E-03 
c  VelocityY    0.46303E+04      13   0.61301E-02   0.25455E-04 
c  VelocityZ    0.46303E+04      13   0.61301E-02   0.43491E-04 
c  TurbEner     0.59790E+01      12   0.71237E-04   0.66207E-09 
c  Dissip       0.14400E+01      13   0.50160E-03   0.36323E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.08           54544           26777           27271
v  Velocity[x]            0.29269          2.1404         0.90805         0.90984
v  Velocity[y]           -0.36699         0.70378      0.00054861       0.0003249
v  Velocity[z]            -0.4203         0.50473      -0.0012608      -0.0013797
v  TurbEner              0.001049        0.014892       0.0032883       0.0033472
v  Dissip               9.203e-05        0.029795      0.00045176       0.0003905
v  TurbVisc               0.17082           11.34          4.7158          5.2769
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              555:        0.90426E-01

===============================================================


 INSTANT    0.556000000E+03   TIME STEP NUMBER             556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002050E+04
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 :  0.23782E+00 0.13251E+01
   Friction velocity        uet   :  0.14225E-01 0.78987E-01
   Friction velocity        uk    :  0.17740E-01 0.38806E-01
   Dimensionless distance   yplus :  0.43591E+03 0.95356E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61062E+01      56   0.13279E-02   0.20020E-01 
c  VelocityX    0.46302E+04      12   0.69193E-02   0.27299E-03 
c  VelocityY    0.46302E+04      12   0.69193E-02   0.49363E-04 
c  VelocityZ    0.46302E+04      12   0.69193E-02   0.35443E-04 
c  TurbEner     0.59801E+01      12   0.61219E-04   0.54474E-09 
c  Dissip       0.14634E+01      15   0.79215E-03   0.14176E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.84           54552           26777           27272
v  Velocity[x]            0.29278          2.1797         0.90805         0.90982
v  Velocity[y]           -0.38237         0.69139      0.00054151      0.00032205
v  Velocity[z]           -0.42177         0.51185      -0.0012504      -0.0013723
v  TurbEner             0.0010496        0.014977       0.0032885       0.0033473
v  Dissip              9.2085e-05        0.030129      0.00045199      0.00039066
v  TurbVisc                0.1706          11.389          4.7157          5.2768
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              556:        0.89586E-01

===============================================================


 INSTANT    0.557000000E+03   TIME STEP NUMBER             557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999589E+04
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 :  0.23771E+00 0.12195E+01
   Friction velocity        uet   :  0.14219E-01 0.72572E-01
   Friction velocity        uk    :  0.17745E-01 0.38751E-01
   Dimensionless distance   yplus :  0.43524E+03 0.95388E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61678E+01      59   0.17350E-02   0.20224E-01 
c  VelocityX    0.46301E+04      12   0.70159E-02   0.41637E-03 
c  VelocityY    0.46301E+04      12   0.70159E-02   0.30919E-04 
c  VelocityZ    0.46301E+04      12   0.70159E-02   0.47608E-04 
c  TurbEner     0.59807E+01      13   0.11754E-03   0.12380E-08 
c  Dissip       0.14832E+01      16   0.21562E-02   0.54214E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.14           54543           26777           27271
v  Velocity[x]            0.29304          2.0153         0.90807         0.90985
v  Velocity[y]           -0.36686         0.70133      0.00054452      0.00032387
v  Velocity[z]           -0.42024         0.50573      -0.0012584      -0.0013754
v  TurbEner             0.0010508        0.015575       0.0032887       0.0033475
v  Dissip              9.2096e-05        0.031815      0.00045229      0.00039089
v  TurbVisc               0.17021          11.373          4.7158          5.2769
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              557:        0.89788E-01

===============================================================


 INSTANT    0.558000000E+03   TIME STEP NUMBER             558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000925E+04
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 :  0.23789E+00 0.13235E+01
   Friction velocity        uet   :  0.14230E-01 0.78884E-01
   Friction velocity        uk    :  0.17755E-01 0.38800E-01
   Dimensionless distance   yplus :  0.43609E+03 0.95393E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60232E+01      55   0.15874E-02   0.19763E-01 
c  VelocityX    0.46301E+04      12   0.65908E-02   0.35920E-03 
c  VelocityY    0.46301E+04      12   0.65908E-02   0.29687E-04 
c  VelocityZ    0.46301E+04      12   0.65908E-02   0.56149E-04 
c  TurbEner     0.59795E+01      14   0.13595E-03   0.23041E-08 
c  Dissip       0.14556E+01      16   0.19336E-02   0.59446E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.24           54518           26778           27272
v  Velocity[x]            0.29253          2.0905         0.90805         0.90983
v  Velocity[y]           -0.38281         0.69551      0.00054465      0.00032695
v  Velocity[z]           -0.42144         0.51056      -0.0012479      -0.0013672
v  TurbEner             0.0010455        0.014996       0.0032885       0.0033474
v  Dissip              9.2083e-05         0.03062      0.00045217      0.00039082
v  TurbVisc               0.17064          11.376          4.7158          5.2768
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              558:        0.89777E-01

===============================================================


 INSTANT    0.559000000E+03   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998455E+04
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 :  0.23771E+00 0.12173E+01
   Friction velocity        uet   :  0.14219E-01 0.72562E-01
   Friction velocity        uk    :  0.17710E-01 0.38755E-01
   Dimensionless distance   yplus :  0.43537E+03 0.95354E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61690E+01      54   0.12384E-02   0.20224E-01 
c  VelocityX    0.46301E+04      12   0.70311E-02   0.39576E-03 
c  VelocityY    0.46301E+04      12   0.70311E-02   0.24215E-04 
c  VelocityZ    0.46301E+04      12   0.70311E-02   0.40305E-04 
c  TurbEner     0.59787E+01      12   0.62414E-04   0.85827E-09 
c  Dissip       0.14615E+01      14   0.46471E-03   0.37680E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.75           54526           26777           27271
v  Velocity[x]            0.29251          2.1389         0.90806         0.90983
v  Velocity[y]           -0.36739         0.70285      0.00054353      0.00032218
v  Velocity[z]           -0.42012         0.50432      -0.0012601      -0.0013762
v  TurbEner             0.0010468        0.014866       0.0032884       0.0033473
v  Dissip              9.2002e-05        0.030374      0.00045218      0.00039082
v  TurbVisc               0.17009          11.351          4.7156          5.2767
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              559:        0.88964E-01

===============================================================


 INSTANT    0.560000000E+03   TIME STEP NUMBER             560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000670E+04
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 :  0.23790E+00 0.13245E+01
   Friction velocity        uet   :  0.14231E-01 0.78951E-01
   Friction velocity        uk    :  0.17721E-01 0.38763E-01
   Dimensionless distance   yplus :  0.43482E+03 0.95370E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60030E+01      63   0.11355E-02   0.19670E-01 
c  VelocityX    0.46302E+04      12   0.77515E-02   0.35709E-03 
c  VelocityY    0.46302E+04      12   0.77515E-02   0.23980E-04 
c  VelocityZ    0.46302E+04      12   0.77515E-02   0.33591E-04 
c  TurbEner     0.59794E+01      13   0.70253E-04   0.89429E-09 
c  Dissip       0.14814E+01      15   0.68442E-03   0.11505E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.21           54534           26777           27271
v  Velocity[x]             0.2932          2.1807         0.90805         0.90983
v  Velocity[y]           -0.38222         0.69555      0.00054013      0.00031892
v  Velocity[z]           -0.41964         0.51184      -0.0012527      -0.0013728
v  TurbEner             0.0010455        0.014923       0.0032883       0.0033472
v  Dissip              9.1992e-05        0.030558      0.00045231       0.0003909
v  TurbVisc               0.16979          11.344          4.7155          5.2766
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              560:        0.90503E-01

===============================================================


 INSTANT    0.561000000E+03   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001354E+04
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 :  0.23739E+00 0.12508E+01
   Friction velocity        uet   :  0.14201E-01 0.73073E-01
   Friction velocity        uk    :  0.17710E-01 0.38795E-01
   Dimensionless distance   yplus :  0.43498E+03 0.95339E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57183E+01      54   0.15238E-02   0.18757E-01 
c  VelocityX    0.46300E+04      12   0.68328E-02   0.36832E-03 
c  VelocityY    0.46300E+04      12   0.68328E-02   0.61751E-04 
c  VelocityZ    0.46300E+04      12   0.68328E-02   0.10047E-03 
c  TurbEner     0.59798E+01      13   0.11724E-03   0.11850E-08 
c  Dissip       0.14935E+01      16   0.17443E-02   0.33728E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -177           54542           26776           27271
v  Velocity[x]            0.29287          2.0188         0.90804         0.90982
v  Velocity[y]           -0.36613         0.70207      0.00054493      0.00032259
v  Velocity[z]           -0.42133         0.50649       -0.001259      -0.0013787
v  TurbEner             0.0010417        0.015486       0.0032883       0.0033472
v  Dissip              9.1964e-05        0.031925      0.00045251      0.00039105
v  TurbVisc               0.16985          11.376          4.7155          5.2765
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              561:        0.89248E-01

===============================================================


 INSTANT    0.562000000E+03   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000778E+04
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 :  0.23772E+00 0.13256E+01
   Friction velocity        uet   :  0.14220E-01 0.79014E-01
   Friction velocity        uk    :  0.17678E-01 0.38788E-01
   Dimensionless distance   yplus :  0.43459E+03 0.95311E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65252E+01      53   0.13376E-02   0.21396E-01 
c  VelocityX    0.46299E+04      12   0.71658E-02   0.49608E-03 
c  VelocityY    0.46299E+04      12   0.71658E-02   0.22991E-04 
c  VelocityZ    0.46299E+04      12   0.71658E-02   0.57587E-04 
c  TurbEner     0.59780E+01      13   0.10481E-03   0.16251E-08 
c  Dissip       0.14480E+01      17   0.15683E-02   0.59526E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.53           54550           26777           27271
v  Velocity[x]            0.29239          1.7259         0.90804         0.90982
v  Velocity[y]            -0.3823         0.69355      0.00053561      0.00031657
v  Velocity[z]            -0.4209         0.51103      -0.0012562      -0.0013763
v  TurbEner             0.0010415        0.015383        0.003288       0.0033471
v  Dissip              9.1983e-05        0.031806      0.00045223      0.00039088
v  TurbVisc               0.16949          11.353          4.7154          5.2764
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              562:        0.88006E-01

===============================================================


 INSTANT    0.563000000E+03   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998566E+04
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 :  0.23796E+00 0.12165E+01
   Friction velocity        uet   :  0.14234E-01 0.72510E-01
   Friction velocity        uk    :  0.17676E-01 0.38789E-01
   Dimensionless distance   yplus :  0.43375E+03 0.95319E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61881E+01      55   0.13425E-02   0.20290E-01 
c  VelocityX    0.46300E+04      12   0.73440E-02   0.38331E-03 
c  VelocityY    0.46300E+04      12   0.73440E-02   0.25798E-04 
c  VelocityZ    0.46300E+04      12   0.73440E-02   0.39757E-04 
c  TurbEner     0.59737E+01      15   0.38309E-03   0.77821E-08 
c  Dissip       0.13067E+01      18   0.78533E-02   0.43595E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.1           54541           26777           27271
v  Velocity[x]            0.29297          1.8694         0.90807         0.90985
v  Velocity[y]           -0.36775         0.70113      0.00053983       0.0003195
v  Velocity[z]           -0.42053         0.50412      -0.0012576      -0.0013761
v  TurbEner             0.0010425        0.013269       0.0032876       0.0033467
v  Dissip              9.2016e-05        0.026399       0.0004515      0.00039033
v  TurbVisc                 0.169          11.349          4.7152          5.2763
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              563:        0.89725E-01

===============================================================


 INSTANT    0.564000000E+03   TIME STEP NUMBER             564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999328E+04
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 :  0.23779E+00 0.13231E+01
   Friction velocity        uet   :  0.14223E-01 0.78867E-01
   Friction velocity        uk    :  0.17685E-01 0.38804E-01
   Dimensionless distance   yplus :  0.43447E+03 0.95301E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58736E+01      53   0.15076E-02   0.19267E-01 
c  VelocityX    0.46300E+04      12   0.66180E-02   0.36756E-03 
c  VelocityY    0.46300E+04      12   0.66180E-02   0.21765E-04 
c  VelocityZ    0.46300E+04      12   0.66180E-02   0.38367E-04 
c  TurbEner     0.59729E+01      14   0.15318E-03   0.27698E-08 
c  Dissip       0.12543E+01      18   0.36128E-02   0.12386E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.29           54517           26777           27272
v  Velocity[x]            0.29302          1.9931         0.90805         0.90983
v  Velocity[y]           -0.38249          0.6936      0.00054495      0.00032863
v  Velocity[z]           -0.42241         0.51171       -0.001247      -0.0013686
v  TurbEner             0.0010369        0.012569       0.0032874       0.0033466
v  Dissip              9.2062e-05        0.024135      0.00045082      0.00038986
v  TurbVisc               0.16933           11.32          4.7152          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              564:        0.89590E-01

===============================================================


 INSTANT    0.565000000E+03   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998639E+04
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 :  0.23755E+00 0.12161E+01
   Friction velocity        uet   :  0.14209E-01 0.72501E-01
   Friction velocity        uk    :  0.17637E-01 0.38720E-01
   Dimensionless distance   yplus :  0.43364E+03 0.95314E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64917E+01      53   0.13029E-02   0.21290E-01 
c  VelocityX    0.46300E+04      12   0.66093E-02   0.32808E-03 
c  VelocityY    0.46300E+04      12   0.66093E-02   0.34824E-04 
c  VelocityZ    0.46300E+04      12   0.66093E-02   0.31515E-04 
c  TurbEner     0.59716E+01      13   0.10102E-03   0.20625E-08 
c  Dissip       0.12218E+01      18   0.22230E-02   0.78664E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.83           54523           26777           27271
v  Velocity[x]            0.29273          2.0618         0.90804         0.90982
v  Velocity[y]           -0.36664         0.70112      0.00054203       0.0003215
v  Velocity[z]           -0.41936         0.50597      -0.0012604      -0.0013806
v  TurbEner             0.0010381         0.01252       0.0032871       0.0033463
v  Dissip              9.2075e-05        0.023269      0.00045012      0.00038938
v  TurbVisc               0.16868          11.328          4.7152          5.2763
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              565:        0.89264E-01

===============================================================


 INSTANT    0.566000000E+03   TIME STEP NUMBER             566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000590E+04
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 :  0.23766E+00 0.13247E+01
   Friction velocity        uet   :  0.14215E-01 0.78965E-01
   Friction velocity        uk    :  0.17647E-01 0.38747E-01
   Dimensionless distance   yplus :  0.43307E+03 0.95343E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60299E+01      56   0.13379E-02   0.19765E-01 
c  VelocityX    0.46300E+04      12   0.75622E-02   0.34087E-03 
c  VelocityY    0.46300E+04      12   0.75622E-02   0.40095E-04 
c  VelocityZ    0.46300E+04      12   0.75622E-02   0.56733E-04 
c  TurbEner     0.59720E+01      13   0.82355E-04   0.98544E-09 
c  Dissip       0.12159E+01      17   0.96381E-03   0.20323E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.58           54524           26777           27271
v  Velocity[x]            0.29277          2.1164         0.90804         0.90982
v  Velocity[y]            -0.3823          0.6946      0.00055039      0.00033112
v  Velocity[z]           -0.42043         0.51107      -0.0012458      -0.0013693
v  TurbEner             0.0010372        0.012823       0.0032868       0.0033461
v  Dissip               9.208e-05        0.023232      0.00044959      0.00038901
v  TurbVisc               0.16833          11.367          4.7152          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              566:        0.89449E-01

===============================================================


 INSTANT    0.567000000E+03   TIME STEP NUMBER             567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001791E+04
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 :  0.23759E+00 0.12141E+01
   Friction velocity        uet   :  0.14211E-01 0.72330E-01
   Friction velocity        uk    :  0.17640E-01 0.38788E-01
   Dimensionless distance   yplus :  0.43332E+03 0.95269E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73049E+01      65   0.16105E-02   0.23957E-01 
c  VelocityX    0.46301E+04      13   0.72491E-02   0.40770E-03 
c  VelocityY    0.46301E+04      13   0.72491E-02   0.40208E-04 
c  VelocityZ    0.46301E+04      13   0.72491E-02   0.50536E-04 
c  TurbEner     0.59726E+01      13   0.87899E-04   0.12364E-08 
c  Dissip       0.12224E+01      16   0.47689E-03   0.60147E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.97           54505           26776           27270
v  Velocity[x]            0.29268          2.1582         0.90808         0.90985
v  Velocity[y]           -0.36697         0.70266      0.00054229      0.00032191
v  Velocity[z]           -0.42028         0.50476      -0.0012506      -0.0013703
v  TurbEner             0.0010333        0.013182       0.0032866       0.0033459
v  Dissip              9.2114e-05        0.023437      0.00044921      0.00038875
v  TurbVisc               0.16841          11.349          4.7152          5.2762
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              567:        0.92137E-01

===============================================================


 INSTANT    0.568000000E+03   TIME STEP NUMBER             568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001217E+04
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 :  0.23803E+00 0.13254E+01
   Friction velocity        uet   :  0.14237E-01 0.79006E-01
   Friction velocity        uk    :  0.17607E-01 0.38830E-01
   Dimensionless distance   yplus :  0.43288E+03 0.95274E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62490E+01      63   0.12263E-02   0.20481E-01 
c  VelocityX    0.46302E+04      12   0.77220E-02   0.40298E-03 
c  VelocityY    0.46302E+04      12   0.77220E-02   0.29919E-04 
c  VelocityZ    0.46302E+04      12   0.77220E-02   0.36380E-04 
c  TurbEner     0.59734E+01      13   0.11323E-03   0.19359E-08 
c  Dissip       0.12462E+01      16   0.10646E-02   0.15727E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.63           54516           26776           27271
v  Velocity[x]            0.29276          2.1933         0.90807         0.90985
v  Velocity[y]           -0.38233         0.69178       0.0005416      0.00032262
v  Velocity[z]           -0.42097          0.5118      -0.0012478      -0.0013703
v  TurbEner             0.0010332        0.013683       0.0032864       0.0033458
v  Dissip              9.2112e-05         0.02416      0.00044903      0.00038861
v  TurbVisc               0.16802          11.331          4.7151          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              568:        0.90624E-01

===============================================================


 INSTANT    0.569000000E+03   TIME STEP NUMBER             569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998823E+04
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 :  0.23779E+00 0.12170E+01
   Friction velocity        uet   :  0.14222E-01 0.72546E-01
   Friction velocity        uk    :  0.17606E-01 0.38829E-01
   Dimensionless distance   yplus :  0.43198E+03 0.95311E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75202E+01      58   0.16661E-02   0.24650E-01 
c  VelocityX    0.46300E+04      12   0.68358E-02   0.41064E-03 
c  VelocityY    0.46300E+04      12   0.68358E-02   0.40848E-04 
c  VelocityZ    0.46300E+04      12   0.68358E-02   0.11144E-03 
c  TurbEner     0.59748E+01      14   0.15167E-03   0.25307E-08 
c  Dissip       0.12704E+01      17   0.21865E-02   0.54164E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.41           54531           26776           27270
v  Velocity[x]            0.29304          2.0299         0.90805         0.90983
v  Velocity[y]           -0.36687         0.69966      0.00055192      0.00032818
v  Velocity[z]           -0.42128         0.50577      -0.0012461      -0.0013684
v  TurbEner             0.0010337        0.014543       0.0032864       0.0033458
v  Dissip              9.2129e-05          0.0258      0.00044905      0.00038865
v  TurbVisc               0.16752          11.357          4.7152          5.2762
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              569:        0.89855E-01

===============================================================


 INSTANT    0.570000000E+03   TIME STEP NUMBER             570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001226E+04
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 :  0.23766E+00 0.13239E+01
   Friction velocity        uet   :  0.14214E-01 0.78917E-01
   Friction velocity        uk    :  0.17610E-01 0.38807E-01
   Dimensionless distance   yplus :  0.43264E+03 0.95295E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69431E+01      56   0.14776E-02   0.22783E-01 
c  VelocityX    0.46300E+04      12   0.69933E-02   0.49534E-03 
c  VelocityY    0.46300E+04      12   0.69933E-02   0.48580E-04 
c  VelocityZ    0.46300E+04      12   0.69933E-02   0.52726E-04 
c  TurbEner     0.59740E+01      13   0.97573E-04   0.14453E-08 
c  Dissip       0.12481E+01      16   0.12257E-02   0.27193E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.07           54543           26777           27271
v  Velocity[x]            0.29262          1.7235         0.90804         0.90982
v  Velocity[y]            -0.3828         0.69279      0.00053522      0.00031445
v  Velocity[z]           -0.42135          0.5105      -0.0012608      -0.0013815
v  TurbEner             0.0010277        0.014712       0.0032864       0.0033457
v  Dissip              9.2081e-05        0.026229       0.0004488      0.00038849
v  TurbVisc               0.16784          11.334          4.7152          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              570:        0.89294E-01

===============================================================


 INSTANT    0.571000000E+03   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998408E+04
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 :  0.23793E+00 0.12437E+01
   Friction velocity        uet   :  0.14230E-01 0.72537E-01
   Friction velocity        uk    :  0.17559E-01 0.38704E-01
   Dimensionless distance   yplus :  0.43174E+03 0.95310E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61479E+01      55   0.12189E-02   0.20158E-01 
c  VelocityX    0.46300E+04      13   0.65597E-02   0.43258E-03 
c  VelocityY    0.46300E+04      13   0.65597E-02   0.29064E-04 
c  VelocityZ    0.46300E+04      13   0.65597E-02   0.34593E-04 
c  TurbEner     0.59706E+01      15   0.30258E-03   0.65543E-08 
c  Dissip       0.11553E+01      18   0.57814E-02   0.23703E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.33           54550           26777           27271
v  Velocity[x]             0.2928          1.8815         0.90804         0.90983
v  Velocity[y]           -0.36736         0.70135      0.00054488      0.00032122
v  Velocity[z]           -0.42096         0.50432      -0.0012609      -0.0013812
v  TurbEner             0.0010276        0.012847       0.0032861       0.0033455
v  Dissip              9.2047e-05        0.022196      0.00044823      0.00038807
v  TurbVisc               0.16721          11.345          4.7153          5.2762
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              571:        0.90020E-01

===============================================================


 INSTANT    0.572000000E+03   TIME STEP NUMBER             572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998236E+04
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 :  0.23763E+00 0.13232E+01
   Friction velocity        uet   :  0.14212E-01 0.78874E-01
   Friction velocity        uk    :  0.17558E-01 0.38620E-01
   Dimensionless distance   yplus :  0.43092E+03 0.95340E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58443E+01      52   0.13928E-02   0.19163E-01 
c  VelocityX    0.46301E+04      12   0.67824E-02   0.34650E-03 
c  VelocityY    0.46301E+04      12   0.67824E-02   0.25371E-04 
c  VelocityZ    0.46301E+04      12   0.67824E-02   0.37039E-04 
c  TurbEner     0.59703E+01      13   0.10561E-03   0.15506E-08 
c  Dissip       0.11275E+01      17   0.22662E-02   0.48222E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.14           54544           26777           27272
v  Velocity[x]            0.29282          1.9899         0.90807         0.90985
v  Velocity[y]           -0.38226         0.69442      0.00054404      0.00032511
v  Velocity[z]           -0.41929         0.51192      -0.0012535      -0.0013731
v  TurbEner             0.0010261        0.012334       0.0032861       0.0033455
v  Dissip              9.2001e-05        0.020705      0.00044775      0.00038775
v  TurbVisc                0.1668          11.324          4.7153          5.2762
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              572:        0.89030E-01

===============================================================


 INSTANT    0.573000000E+03   TIME STEP NUMBER             573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999099E+04
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 :  0.23768E+00 0.12163E+01
   Friction velocity        uet   :  0.14215E-01 0.72511E-01
   Friction velocity        uk    :  0.17545E-01 0.38730E-01
   Dimensionless distance   yplus :  0.43104E+03 0.95288E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58252E+01      66   0.15170E-02   0.19120E-01 
c  VelocityX    0.46302E+04      12   0.68870E-02   0.32553E-03 
c  VelocityY    0.46302E+04      12   0.68870E-02   0.22626E-04 
c  VelocityZ    0.46302E+04      12   0.68870E-02   0.39247E-04 
c  TurbEner     0.59707E+01      13   0.78711E-04   0.13204E-08 
c  Dissip       0.11166E+01      17   0.10217E-02   0.18547E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.95           54520           26778           27272
v  Velocity[x]            0.29272          2.0696         0.90807         0.90984
v  Velocity[y]           -0.36614         0.70106      0.00055264      0.00033265
v  Velocity[z]           -0.42031         0.50649      -0.0012485      -0.0013691
v  TurbEner             0.0010217        0.012381       0.0032861       0.0033455
v  Dissip              9.1992e-05         0.02032      0.00044735      0.00038747
v  TurbVisc               0.16692          11.322          4.7155          5.2763
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              573:        0.92046E-01

===============================================================


 INSTANT    0.574000000E+03   TIME STEP NUMBER             574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999525E+04
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 :  0.23781E+00 0.13258E+01
   Friction velocity        uet   :  0.14224E-01 0.79028E-01
   Friction velocity        uk    :  0.17508E-01 0.38795E-01
   Dimensionless distance   yplus :  0.43057E+03 0.95291E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56461E+01      53   0.10604E-02   0.18509E-01 
c  VelocityX    0.46302E+04      12   0.73314E-02   0.35071E-03 
c  VelocityY    0.46302E+04      12   0.73314E-02   0.27482E-04 
c  VelocityZ    0.46302E+04      12   0.73314E-02   0.42039E-04 
c  TurbEner     0.59708E+01      13   0.74745E-04   0.11068E-08 
c  Dissip       0.11193E+01      16   0.53894E-03   0.61265E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.88           54530           26778           27272
v  Velocity[x]            0.29291          2.1166         0.90805         0.90983
v  Velocity[y]           -0.38233         0.69479      0.00054837      0.00032925
v  Velocity[z]           -0.42179         0.51107       -0.001251      -0.0013742
v  TurbEner             0.0010218        0.012696       0.0032861       0.0033455
v  Dissip               9.201e-05        0.020447        0.000447      0.00038723
v  TurbVisc               0.16666          11.351          4.7157          5.2764
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              574:        0.88991E-01

===============================================================


 INSTANT    0.575000000E+03   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998515E+04
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 :  0.23764E+00 0.12140E+01
   Friction velocity        uet   :  0.14214E-01 0.72320E-01
   Friction velocity        uk    :  0.17508E-01 0.38781E-01
   Dimensionless distance   yplus :  0.42973E+03 0.95288E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64250E+01      54   0.12768E-02   0.21060E-01 
c  VelocityX    0.46303E+04      12   0.70165E-02   0.38026E-03 
c  VelocityY    0.46303E+04      12   0.70165E-02   0.42396E-04 
c  VelocityZ    0.46303E+04      12   0.70165E-02   0.84624E-04 
c  TurbEner     0.59721E+01      13   0.10082E-03   0.13555E-08 
c  Dissip       0.11341E+01      15   0.73943E-03   0.66827E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.09           54538           26778           27272
v  Velocity[x]            0.29285          2.1566         0.90805         0.90983
v  Velocity[y]           -0.36772         0.70287       0.0005554      0.00033061
v  Velocity[z]           -0.42128         0.50419       -0.001244      -0.0013649
v  TurbEner             0.0010234        0.013159       0.0032863       0.0033456
v  Dissip              9.2046e-05        0.020972      0.00044688      0.00038715
v  TurbVisc               0.16637          11.335          4.7159          5.2766
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              575:        0.89444E-01

===============================================================


 INSTANT    0.576000000E+03   TIME STEP NUMBER             576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000674E+04
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 :  0.23802E+00 0.13255E+01
   Friction velocity        uet   :  0.14237E-01 0.79011E-01
   Friction velocity        uk    :  0.17522E-01 0.38737E-01
   Dimensionless distance   yplus :  0.43056E+03 0.95258E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54090E+01      56   0.13479E-02   0.17750E-01 
c  VelocityX    0.46303E+04      12   0.70919E-02   0.36231E-03 
c  VelocityY    0.46303E+04      12   0.70919E-02   0.24204E-04 
c  VelocityZ    0.46303E+04      12   0.70919E-02   0.38928E-04 
c  TurbEner     0.59734E+01      14   0.14392E-03   0.26148E-08 
c  Dissip       0.11525E+01      17   0.20478E-02   0.44574E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.39           54546           26778           27273
v  Velocity[x]            0.29274          1.9947         0.90806         0.90984
v  Velocity[y]           -0.38245         0.69388      0.00054219      0.00032157
v  Velocity[z]           -0.42152         0.51168      -0.0012551       -0.001379
v  TurbEner             0.0010192        0.014033       0.0032865       0.0033459
v  Dissip              9.2056e-05         0.02252      0.00044694      0.00038721
v  TurbVisc                 0.167          11.347          4.7161          5.2768
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              576:        0.90131E-01

===============================================================


 INSTANT    0.577000000E+03   TIME STEP NUMBER             577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999195E+04
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 :  0.23795E+00 0.12304E+01
   Friction velocity        uet   :  0.14233E-01 0.72484E-01
   Friction velocity        uk    :  0.17486E-01 0.38658E-01
   Dimensionless distance   yplus :  0.42994E+03 0.95276E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58270E+01      56   0.12418E-02   0.19114E-01 
c  VelocityX    0.46304E+04      12   0.67409E-02   0.35197E-03 
c  VelocityY    0.46304E+04      12   0.67409E-02   0.22350E-04 
c  VelocityZ    0.46304E+04      12   0.67409E-02   0.51026E-04 
c  TurbEner     0.59732E+01      13   0.76978E-04   0.92550E-09 
c  Dissip       0.11438E+01      16   0.10130E-02   0.17937E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.92           54554           26778           27272
v  Velocity[x]            0.29286          2.0727         0.90805         0.90984
v  Velocity[y]           -0.36661         0.70053      0.00054877      0.00032464
v  Velocity[z]           -0.42128         0.50605      -0.0012541      -0.0013747
v  TurbEner             0.0010223        0.013791       0.0032866       0.0033459
v  Dissip              9.2087e-05           0.022      0.00044679      0.00038712
v  TurbVisc               0.16676          11.331          4.7164           5.277
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              577:        0.88262E-01

===============================================================


 INSTANT    0.578000000E+03   TIME STEP NUMBER             578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001959E+04
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 :  0.23774E+00 0.13249E+01
   Friction velocity        uet   :  0.14222E-01 0.78971E-01
   Friction velocity        uk    :  0.17513E-01 0.38730E-01
   Dimensionless distance   yplus :  0.42971E+03 0.95270E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62285E+01      55   0.15172E-02   0.20425E-01 
c  VelocityX    0.46304E+04      12   0.71753E-02   0.38322E-03 
c  VelocityY    0.46304E+04      12   0.71753E-02   0.25931E-04 
c  VelocityZ    0.46304E+04      12   0.71753E-02   0.52664E-04 
c  TurbEner     0.59745E+01      13   0.76607E-04   0.11236E-08 
c  Dissip       0.11593E+01      15   0.60930E-03   0.84657E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.28           54546           26778           27272
v  Velocity[x]            0.29298          2.1215         0.90807         0.90985
v  Velocity[y]           -0.38233         0.69219      0.00054213      0.00032107
v  Velocity[z]            -0.4193         0.51103      -0.0012498      -0.0013716
v  TurbEner             0.0010242        0.013954        0.003287       0.0033462
v  Dissip              9.2064e-05        0.022239       0.0004469       0.0003872
v  TurbVisc               0.16689          11.334          4.7166          5.2772
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              578:        0.89553E-01

===============================================================


 INSTANT    0.579000000E+03   TIME STEP NUMBER             579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999750E+04
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 :  0.23747E+00 0.12159E+01
   Friction velocity        uet   :  0.14206E-01 0.72482E-01
   Friction velocity        uk    :  0.17529E-01 0.38798E-01
   Dimensionless distance   yplus :  0.43041E+03 0.95210E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67460E+01      60   0.15897E-02   0.22132E-01 
c  VelocityX    0.46305E+04      13   0.68100E-02   0.37523E-03 
c  VelocityY    0.46305E+04      13   0.68100E-02   0.75295E-04 
c  VelocityZ    0.46305E+04      13   0.68100E-02   0.10623E-03 
c  TurbEner     0.59764E+01      13   0.10003E-03   0.18171E-08 
c  Dissip       0.11886E+01      17   0.11855E-02   0.28459E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.24           54522           26778           27272
v  Velocity[x]            0.29283          2.1647         0.90806         0.90984
v  Velocity[y]           -0.36705         0.70036       0.0005565      0.00033622
v  Velocity[z]           -0.42205         0.50471      -0.0012299      -0.0013527
v  TurbEner             0.0010229         0.01429       0.0032874       0.0033465
v  Dissip              9.2075e-05        0.022888      0.00044719       0.0003874
v  TurbVisc               0.16753          11.313          4.7169          5.2775
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              579:        0.90168E-01

===============================================================


 INSTANT    0.580000000E+03   TIME STEP NUMBER             580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000871E+04
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 :  0.23747E+00 0.13230E+01
   Friction velocity        uet   :  0.14206E-01 0.78865E-01
   Friction velocity        uk    :  0.17518E-01 0.38792E-01
   Dimensionless distance   yplus :  0.43041E+03 0.95251E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58598E+01      57   0.14418E-02   0.19230E-01 
c  VelocityX    0.46305E+04      12   0.65923E-02   0.39702E-03 
c  VelocityY    0.46305E+04      12   0.65923E-02   0.28076E-04 
c  VelocityZ    0.46305E+04      12   0.65923E-02   0.52230E-04 
c  TurbEner     0.59769E+01      14   0.13797E-03   0.28557E-08 
c  Dissip       0.12158E+01      17   0.22646E-02   0.69704E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -171.2           54529           26779           27273
v  Velocity[x]            0.29258          2.0001         0.90805         0.90983
v  Velocity[y]            -0.3824          0.6936      0.00054692      0.00032773
v  Velocity[z]           -0.42058         0.51189      -0.0012443      -0.0013689
v  TurbEner             0.0010263        0.015091       0.0032878       0.0033468
v  Dissip              9.2029e-05        0.024601      0.00044761      0.00038769
v  TurbVisc               0.16768          11.304          4.7171          5.2777
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              580:        0.89784E-01

===============================================================


 INSTANT    0.581000000E+03   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998206E+04
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 :  0.23813E+00 0.12371E+01
   Friction velocity        uet   :  0.14245E-01 0.72464E-01
   Friction velocity        uk    :  0.17547E-01 0.38782E-01
   Dimensionless distance   yplus :  0.43016E+03 0.95292E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57586E+01      54   0.13095E-02   0.18885E-01 
c  VelocityX    0.46305E+04      12   0.61002E-02   0.29534E-03 
c  VelocityY    0.46305E+04      12   0.61002E-02   0.27007E-04 
c  VelocityZ    0.46305E+04      12   0.61002E-02   0.45835E-04 
c  TurbEner     0.59762E+01      13   0.94716E-04   0.15478E-08 
c  Dissip       0.12071E+01      16   0.10554E-02   0.21583E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.74           54538           26778           27273
v  Velocity[x]            0.29294          2.0755         0.90805         0.90984
v  Velocity[y]           -0.36853         0.70092      0.00054553      0.00032373
v  Velocity[z]           -0.42093         0.50654      -0.0012401      -0.0013628
v  TurbEner             0.0010315        0.014685        0.003288       0.0033469
v  Dissip              9.1989e-05        0.024029      0.00044771      0.00038776
v  TurbVisc               0.16785          11.335          4.7173          5.2779
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              581:        0.89178E-01

===============================================================


 INSTANT    0.582000000E+03   TIME STEP NUMBER             582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000768E+04
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 :  0.23770E+00 0.13255E+01
   Friction velocity        uet   :  0.14220E-01 0.79021E-01
   Friction velocity        uk    :  0.17591E-01 0.38722E-01
   Dimensionless distance   yplus :  0.43159E+03 0.95333E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56093E+01      51   0.12560E-02   0.18403E-01 
c  VelocityX    0.46306E+04      13   0.67579E-02   0.31156E-03 
c  VelocityY    0.46306E+04      13   0.67579E-02   0.25041E-04 
c  VelocityZ    0.46306E+04      13   0.67579E-02   0.51786E-04 
c  TurbEner     0.59772E+01      13   0.62731E-04   0.74760E-09 
c  Dissip       0.12263E+01      15   0.61956E-03   0.99153E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.9           54547           26779           27273
v  Velocity[x]            0.29266          2.1256         0.90806         0.90985
v  Velocity[y]           -0.38329         0.69431       0.0005368       0.0003169
v  Velocity[z]           -0.42219         0.51326      -0.0012544      -0.0013785
v  TurbEner             0.0010318        0.014715       0.0032884       0.0033471
v  Dissip              9.2048e-05        0.024273      0.00044797      0.00038792
v  TurbVisc               0.16893          11.385          4.7175          5.2781
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              582:        0.89407E-01

===============================================================


 INSTANT    0.583000000E+03   TIME STEP NUMBER             583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998033E+04
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 :  0.23771E+00 0.12141E+01
   Friction velocity        uet   :  0.14220E-01 0.72330E-01
   Friction velocity        uk    :  0.17594E-01 0.38702E-01
   Dimensionless distance   yplus :  0.43193E+03 0.95382E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.76932E+01      69   0.14742E-02   0.25218E-01 
c  VelocityX    0.46307E+04      12   0.73834E-02   0.35216E-03 
c  VelocityY    0.46307E+04      12   0.73834E-02   0.55701E-04 
c  VelocityZ    0.46307E+04      12   0.73834E-02   0.97949E-04 
c  TurbEner     0.59786E+01      13   0.84125E-04   0.11067E-08 
c  Dissip       0.12597E+01      17   0.11875E-02   0.31944E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.59           54555           26779           27273
v  Velocity[x]            0.29288          2.1719         0.90806         0.90983
v  Velocity[y]           -0.36698         0.70266      0.00055155      0.00032657
v  Velocity[z]           -0.42008         0.50732      -0.0012401      -0.0013622
v  TurbEner             0.0010394        0.014921       0.0032886       0.0033473
v  Dissip              9.2102e-05        0.024884      0.00044838      0.00038818
v  TurbVisc               0.16926          11.378          4.7178          5.2784
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              583:        0.99624E-01

===============================================================


 INSTANT    0.584000000E+03   TIME STEP NUMBER             584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999882E+04
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 :  0.23755E+00 0.13247E+01
   Friction velocity        uet   :  0.14210E-01 0.78972E-01
   Friction velocity        uk    :  0.17658E-01 0.38763E-01
   Dimensionless distance   yplus :  0.43266E+03 0.95358E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75843E+01      64   0.17818E-02   0.24881E-01 
c  VelocityX    0.46305E+04      12   0.72619E-02   0.50133E-03 
c  VelocityY    0.46305E+04      12   0.72619E-02   0.69092E-04 
c  VelocityZ    0.46305E+04      12   0.72619E-02   0.51873E-04 
c  TurbEner     0.59797E+01      14   0.12772E-03   0.21705E-08 
c  Dissip       0.12815E+01      17   0.22096E-02   0.66537E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.55           54548           26780           27275
v  Velocity[x]            0.29281          1.9944         0.90808         0.90987
v  Velocity[y]           -0.38267         0.69246      0.00054587      0.00032502
v  Velocity[z]           -0.42075         0.51211      -0.0012493      -0.0013722
v  TurbEner             0.0010451        0.015681       0.0032893       0.0033477
v  Dissip              9.2135e-05        0.026614      0.00044892      0.00038855
v  TurbVisc               0.16993          11.331           4.718          5.2786
v  total_pressure           83077      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              584:        0.93623E-01

===============================================================


 INSTANT    0.585000000E+03   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998448E+04
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 :  0.23763E+00 0.12539E+01
   Friction velocity        uet   :  0.14214E-01 0.73189E-01
   Friction velocity        uk    :  0.17707E-01 0.38784E-01
   Dimensionless distance   yplus :  0.43424E+03 0.95357E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62802E+01      54   0.15006E-02   0.20602E-01 
c  VelocityX    0.46307E+04      12   0.66819E-02   0.39715E-03 
c  VelocityY    0.46307E+04      12   0.66819E-02   0.39729E-04 
c  VelocityZ    0.46307E+04      12   0.66819E-02   0.34451E-04 
c  TurbEner     0.59797E+01      14   0.12010E-03   0.21859E-08 
c  Dissip       0.12747E+01      16   0.12007E-02   0.25941E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.77           54522           26780           27274
v  Velocity[x]            0.29261           2.086         0.90806         0.90984
v  Velocity[y]           -0.36746         0.70067      0.00054862      0.00032915
v  Velocity[z]           -0.42214         0.50551      -0.0012411      -0.0013614
v  TurbEner             0.0010479        0.015127       0.0032895       0.0033479
v  Dissip              9.2131e-05        0.025847      0.00044905      0.00038863
v  TurbVisc                 0.171          11.323          4.7183          5.2789
v  total_pressure           83082      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              585:        0.90280E-01

===============================================================


 INSTANT    0.586000000E+03   TIME STEP NUMBER             586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002144E+04
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 :  0.23786E+00 0.13246E+01
   Friction velocity        uet   :  0.14228E-01 0.78959E-01
   Friction velocity        uk    :  0.17730E-01 0.38786E-01
   Dimensionless distance   yplus :  0.43511E+03 0.95359E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69597E+01      53   0.13517E-02   0.22831E-01 
c  VelocityX    0.46307E+04      12   0.76992E-02   0.37808E-03 
c  VelocityY    0.46307E+04      12   0.76992E-02   0.34066E-04 
c  VelocityZ    0.46307E+04      12   0.76992E-02   0.45066E-04 
c  TurbEner     0.59798E+01      13   0.64447E-04   0.98815E-09 
c  Dissip       0.12938E+01      15   0.62601E-03   0.98049E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.36           54529           26780           27275
v  Velocity[x]            0.29267          2.1239         0.90805         0.90984
v  Velocity[y]           -0.38246         0.69363      0.00053916      0.00031952
v  Velocity[z]           -0.42143         0.51241      -0.0012522      -0.0013714
v  TurbEner             0.0010545        0.015164       0.0032899       0.0033481
v  Dissip              9.2109e-05        0.026178      0.00044931      0.00038879
v  TurbVisc               0.17153          11.345          4.7185          5.2791
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              586:        0.91519E-01

===============================================================


 INSTANT    0.587000000E+03   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999393E+04
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 :  0.23794E+00 0.12460E+01
   Friction velocity        uet   :  0.14232E-01 0.72593E-01
   Friction velocity        uk    :  0.17787E-01 0.38741E-01
   Dimensionless distance   yplus :  0.43556E+03 0.95332E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68170E+01      55   0.13911E-02   0.22351E-01 
c  VelocityX    0.46308E+04      12   0.71507E-02   0.43494E-03 
c  VelocityY    0.46308E+04      12   0.71507E-02   0.38903E-04 
c  VelocityZ    0.46308E+04      12   0.71507E-02   0.45379E-04 
c  TurbEner     0.59814E+01      13   0.82183E-04   0.12782E-08 
c  Dissip       0.13277E+01      16   0.11887E-02   0.30885E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.09           54529           26780           27274
v  Velocity[x]            0.29324          2.1634         0.90808         0.90986
v  Velocity[y]           -0.36787         0.70169      0.00054588      0.00032142
v  Velocity[z]           -0.42146         0.50744      -0.0012475      -0.0013694
v  TurbEner             0.0010623         0.01535       0.0032904       0.0033485
v  Dissip              9.2043e-05        0.026877       0.0004498      0.00038911
v  TurbVisc               0.17195          11.327          4.7187          5.2793
v  total_pressure           83081      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              587:        0.92181E-01

===============================================================


 INSTANT    0.588000000E+03   TIME STEP NUMBER             588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001230E+04
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 :  0.23770E+00 0.13243E+01
   Friction velocity        uet   :  0.14218E-01 0.78944E-01
   Friction velocity        uk    :  0.17852E-01 0.38770E-01
   Dimensionless distance   yplus :  0.43765E+03 0.95408E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61070E+01      52   0.15092E-02   0.20047E-01 
c  VelocityX    0.46307E+04      12   0.70486E-02   0.34607E-03 
c  VelocityY    0.46307E+04      12   0.70486E-02   0.31141E-04 
c  VelocityZ    0.46307E+04      12   0.70486E-02   0.50044E-04 
c  TurbEner     0.59825E+01      13   0.80112E-04   0.12572E-08 
c  Dissip       0.13614E+01      16   0.12900E-02   0.34853E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.67           54517           26780           27274
v  Velocity[x]            0.29259           2.183         0.90808         0.90986
v  Velocity[y]           -0.38362         0.69422      0.00053782      0.00031915
v  Velocity[z]           -0.42245         0.51321      -0.0012478       -0.001367
v  TurbEner             0.0010634        0.015576       0.0032908       0.0033488
v  Dissip              9.2038e-05        0.027689      0.00045034      0.00038947
v  TurbVisc               0.17321          11.337           4.719          5.2796
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              588:        0.90445E-01

===============================================================


 INSTANT    0.589000000E+03   TIME STEP NUMBER             589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999864E+04
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 :  0.23763E+00 0.12376E+01
   Friction velocity        uet   :  0.14213E-01 0.72523E-01
   Friction velocity        uk    :  0.17861E-01 0.38746E-01
   Dimensionless distance   yplus :  0.43821E+03 0.95438E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72354E+01      57   0.15565E-02   0.23722E-01 
c  VelocityX    0.46307E+04      13   0.72092E-02   0.36813E-03 
c  VelocityY    0.46307E+04      13   0.72092E-02   0.28462E-04 
c  VelocityZ    0.46307E+04      13   0.72092E-02   0.94875E-04 
c  TurbEner     0.59830E+01      13   0.12193E-03   0.18682E-08 
c  Dissip       0.13955E+01      17   0.23344E-02   0.74386E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.92           54524           26779           27273
v  Velocity[x]            0.29241          2.0322         0.90807         0.90984
v  Velocity[y]           -0.36871         0.70087       0.0005492      0.00032584
v  Velocity[z]           -0.42023         0.50825      -0.0012452      -0.0013662
v  TurbEner             0.0010706        0.016215       0.0032912        0.003349
v  Dissip              9.2048e-05        0.029607      0.00045091      0.00038985
v  TurbVisc               0.17348          11.321          4.7191          5.2797
v  total_pressure           83081      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              589:        0.90763E-01

===============================================================


 INSTANT    0.590000000E+03   TIME STEP NUMBER             590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001799E+04
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 :  0.23758E+00 0.13259E+01
   Friction velocity        uet   :  0.14210E-01 0.79026E-01
   Friction velocity        uk    :  0.17922E-01 0.38780E-01
   Dimensionless distance   yplus :  0.43888E+03 0.95382E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65939E+01      56   0.13355E-02   0.21630E-01 
c  VelocityX    0.46306E+04      12   0.66143E-02   0.32919E-03 
c  VelocityY    0.46306E+04      12   0.66143E-02   0.25995E-04 
c  VelocityZ    0.46306E+04      12   0.66143E-02   0.55370E-04 
c  TurbEner     0.59821E+01      13   0.11090E-03   0.17629E-08 
c  Dissip       0.13844E+01      16   0.11147E-02   0.25561E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.92           54536           26779           27274
v  Velocity[x]            0.29299          2.0899         0.90806         0.90984
v  Velocity[y]           -0.38323          0.6941      0.00054199      0.00032027
v  Velocity[z]           -0.41957          0.5147      -0.0012494       -0.001373
v  TurbEner             0.0010756        0.015706       0.0032914       0.0033492
v  Dissip              9.2008e-05        0.028963      0.00045107      0.00038995
v  TurbVisc               0.17395          11.319          4.7192          5.2798
v  total_pressure           83075      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              590:        0.89399E-01

===============================================================


 INSTANT    0.591000000E+03   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999526E+04
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 :  0.23761E+00 0.12220E+01
   Friction velocity        uet   :  0.14212E-01 0.72334E-01
   Friction velocity        uk    :  0.17964E-01 0.38807E-01
   Dimensionless distance   yplus :  0.44035E+03 0.95329E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61605E+01      57   0.13118E-02   0.20207E-01 
c  VelocityX    0.46307E+04      12   0.67868E-02   0.34911E-03 
c  VelocityY    0.46307E+04      12   0.67868E-02   0.33466E-04 
c  VelocityZ    0.46307E+04      12   0.67868E-02   0.32172E-04 
c  TurbEner     0.59825E+01      13   0.71035E-04   0.79011E-09 
c  Dissip       0.14053E+01      15   0.48908E-03   0.74101E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.54           54548           26779           27273
v  Velocity[x]            0.29284          2.1526         0.90806         0.90984
v  Velocity[y]           -0.36698         0.70219      0.00054392      0.00031988
v  Velocity[z]           -0.42029         0.50851      -0.0012521      -0.0013731
v  TurbEner              0.001076        0.015533       0.0032915       0.0033493
v  Dissip              9.2019e-05        0.029038      0.00045136      0.00039015
v  TurbVisc               0.17482          11.354          4.7193          5.2799
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              591:        0.89818E-01

===============================================================


 INSTANT    0.592000000E+03   TIME STEP NUMBER             592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001629E+04
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 :  0.23798E+00 0.13246E+01
   Friction velocity        uet   :  0.14233E-01 0.78956E-01
   Friction velocity        uk    :  0.17966E-01 0.38822E-01
   Dimensionless distance   yplus :  0.44084E+03 0.95311E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64074E+01      53   0.12428E-02   0.21014E-01 
c  VelocityX    0.46306E+04      12   0.73992E-02   0.36339E-03 
c  VelocityY    0.46306E+04      12   0.73992E-02   0.42154E-04 
c  VelocityZ    0.46306E+04      12   0.73992E-02   0.37645E-04 
c  TurbEner     0.59836E+01      13   0.69551E-04   0.94268E-09 
c  Dissip       0.14372E+01      16   0.12053E-02   0.33280E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.67           54555           26779           27274
v  Velocity[x]            0.29246          2.1726         0.90809         0.90986
v  Velocity[y]           -0.38298         0.69316      0.00053338      0.00031283
v  Velocity[z]           -0.42113         0.51258      -0.0012527      -0.0013743
v  TurbEner             0.0010801        0.015665       0.0032919       0.0033496
v  Dissip              9.1978e-05        0.029705      0.00045185      0.00039049
v  TurbVisc                 0.175          11.338          4.7193          5.2799
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              592:        0.89646E-01

===============================================================


 INSTANT    0.593000000E+03   TIME STEP NUMBER             593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998265E+04
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 :  0.23788E+00 0.12215E+01
   Friction velocity        uet   :  0.14227E-01 0.72444E-01
   Friction velocity        uk    :  0.18001E-01 0.38814E-01
   Dimensionless distance   yplus :  0.44081E+03 0.95271E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71630E+01      58   0.17085E-02   0.23472E-01 
c  VelocityX    0.46306E+04      12   0.77110E-02   0.43572E-03 
c  VelocityY    0.46306E+04      12   0.77110E-02   0.37044E-04 
c  VelocityZ    0.46306E+04      12   0.77110E-02   0.30122E-04 
c  TurbEner     0.59846E+01      13   0.10902E-03   0.13333E-08 
c  Dissip       0.14663E+01      16   0.21623E-02   0.62097E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.08           54546           26778           27272
v  Velocity[x]            0.29299          2.0228         0.90806         0.90984
v  Velocity[y]           -0.36834         0.70077      0.00054525      0.00032428
v  Velocity[z]           -0.42054         0.50532      -0.0012464      -0.0013664
v  TurbEner             0.0010844        0.016178       0.0032922       0.0033498
v  Dissip              9.2013e-05        0.031457      0.00045233      0.00039083
v  TurbVisc               0.17503          11.339          4.7194            5.28
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              593:        0.90553E-01

===============================================================


 INSTANT    0.594000000E+03   TIME STEP NUMBER             594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002137E+04
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 :  0.23716E+00 0.13251E+01
   Friction velocity        uet   :  0.14184E-01 0.78987E-01
   Friction velocity        uk    :  0.18037E-01 0.38815E-01
   Dimensionless distance   yplus :  0.44229E+03 0.95229E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71785E+01      65   0.16765E-02   0.23569E-01 
c  VelocityX    0.46305E+04      12   0.68878E-02   0.39146E-03 
c  VelocityY    0.46305E+04      12   0.68878E-02   0.34461E-04 
c  VelocityZ    0.46305E+04      12   0.68878E-02   0.38744E-04 
c  TurbEner     0.59836E+01      14   0.13985E-03   0.25361E-08 
c  Dissip       0.14440E+01      16   0.16042E-02   0.44385E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.75           54523           26779           27274
v  Velocity[x]            0.29248          2.0854         0.90808         0.90986
v  Velocity[y]           -0.38321         0.69204      0.00053333      0.00031544
v  Velocity[z]            -0.4197         0.51215      -0.0012478      -0.0013669
v  TurbEner             0.0010819        0.015538       0.0032923       0.0033501
v  Dissip              9.2009e-05        0.030417      0.00045239      0.00039089
v  TurbVisc               0.17585          11.315          4.7194            5.28
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              594:        0.91325E-01

===============================================================


 INSTANT    0.595000000E+03   TIME STEP NUMBER             595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997832E+04
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 :  0.23794E+00 0.12397E+01
   Friction velocity        uet   :  0.14231E-01 0.72471E-01
   Friction velocity        uk    :  0.18016E-01 0.38711E-01
   Dimensionless distance   yplus :  0.44221E+03 0.95195E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61534E+01      57   0.12626E-02   0.20174E-01 
c  VelocityX    0.46306E+04      12   0.71700E-02   0.40032E-03 
c  VelocityY    0.46306E+04      12   0.71700E-02   0.23222E-04 
c  VelocityZ    0.46306E+04      12   0.71700E-02   0.36924E-04 
c  TurbEner     0.59833E+01      13   0.77074E-04   0.10622E-08 
c  Dissip       0.14594E+01      14   0.31936E-03   0.30850E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.62           54531           26779           27273
v  Velocity[x]            0.29274          2.1476         0.90807         0.90985
v  Velocity[y]           -0.36667         0.70059      0.00053947      0.00031745
v  Velocity[z]           -0.42171         0.50666       -0.001253      -0.0013733
v  TurbEner             0.0010854        0.015336       0.0032923       0.0033501
v  Dissip              9.1981e-05        0.030346      0.00045258      0.00039102
v  TurbVisc               0.17565          11.323          4.7194          5.2801
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              595:        0.89901E-01

===============================================================


 INSTANT    0.596000000E+03   TIME STEP NUMBER             596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999777E+04
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 :  0.23784E+00 0.13227E+01
   Friction velocity        uet   :  0.14226E-01 0.78845E-01
   Friction velocity        uk    :  0.18045E-01 0.38716E-01
   Dimensionless distance   yplus :  0.44228E+03 0.95170E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70613E+01      54   0.15139E-02   0.23167E-01 
c  VelocityX    0.46305E+04      12   0.69812E-02   0.36011E-03 
c  VelocityY    0.46305E+04      12   0.69812E-02   0.28600E-04 
c  VelocityZ    0.46305E+04      12   0.69812E-02   0.90966E-04 
c  TurbEner     0.59838E+01      13   0.77690E-04   0.10538E-08 
c  Dissip       0.14851E+01      15   0.74150E-03   0.14077E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.55           54539           26779           27273
v  Velocity[x]            0.29313           2.182         0.90807         0.90985
v  Velocity[y]           -0.38233         0.69322      0.00054134      0.00032087
v  Velocity[z]           -0.42054         0.51156      -0.0012427      -0.0013659
v  TurbEner              0.001086        0.015357       0.0032925       0.0033502
v  Dissip              9.1992e-05        0.030623      0.00045289      0.00039125
v  TurbVisc               0.17567           11.36          4.7193          5.2799
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              596:        0.89505E-01

===============================================================


 INSTANT    0.597000000E+03   TIME STEP NUMBER             597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999600E+04
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 :  0.23799E+00 0.12157E+01
   Friction velocity        uet   :  0.14235E-01 0.72479E-01
   Friction velocity        uk    :  0.18050E-01 0.38754E-01
   Dimensionless distance   yplus :  0.44298E+03 0.95163E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57331E+01      51   0.13262E-02   0.18808E-01 
c  VelocityX    0.46304E+04      13   0.63015E-02   0.31813E-03 
c  VelocityY    0.46304E+04      13   0.63015E-02   0.40221E-04 
c  VelocityZ    0.46304E+04      13   0.63015E-02   0.66772E-04 
c  TurbEner     0.59840E+01      13   0.12466E-03   0.13590E-08 
c  Dissip       0.14970E+01      16   0.20207E-02   0.47027E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.44           54546           26778           27273
v  Velocity[x]            0.29259          2.0148         0.90806         0.90983
v  Velocity[y]             -0.367          0.7005      0.00054007      0.00031637
v  Velocity[z]           -0.42088         0.50509      -0.0012509      -0.0013703
v  TurbEner             0.0010824        0.015903       0.0032925       0.0033503
v  Dissip              9.1977e-05        0.032259      0.00045322      0.00039149
v  TurbVisc               0.17598          11.342          4.7192          5.2799
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              597:        0.89835E-01

===============================================================


 INSTANT    0.598000000E+03   TIME STEP NUMBER             598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001315E+04
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 :  0.23779E+00 0.13248E+01
   Friction velocity        uet   :  0.14224E-01 0.78971E-01
   Friction velocity        uk    :  0.18020E-01 0.38792E-01
   Dimensionless distance   yplus :  0.44277E+03 0.95178E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53930E+01      51   0.11124E-02   0.17688E-01 
c  VelocityX    0.46303E+04      12   0.71639E-02   0.31742E-03 
c  VelocityY    0.46303E+04      12   0.71639E-02   0.34225E-04 
c  VelocityZ    0.46303E+04      12   0.71639E-02   0.39589E-04 
c  TurbEner     0.59825E+01      14   0.15721E-03   0.24500E-08 
c  Dissip       0.14664E+01      16   0.21418E-02   0.66558E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.27           54554           26779           27273
v  Velocity[x]             0.2927          2.0985         0.90807         0.90985
v  Velocity[y]           -0.38246         0.69478      0.00054147      0.00032142
v  Velocity[z]           -0.42274         0.51199      -0.0012566      -0.0013787
v  TurbEner             0.0010824        0.015138       0.0032923       0.0033502
v  Dissip               9.199e-05        0.030786      0.00045304      0.00039137
v  TurbVisc               0.17566           11.34           4.719          5.2797
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              598:        0.89336E-01

===============================================================


 INSTANT    0.599000000E+03   TIME STEP NUMBER             599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998812E+04
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 :  0.23766E+00 0.12140E+01
   Friction velocity        uet   :  0.14217E-01 0.72305E-01
   Friction velocity        uk    :  0.18020E-01 0.38804E-01
   Dimensionless distance   yplus :  0.44192E+03 0.95159E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60128E+01      53   0.15142E-02   0.19708E-01 
c  VelocityX    0.46304E+04      12   0.74003E-02   0.35487E-03 
c  VelocityY    0.46304E+04      12   0.74003E-02   0.24194E-04 
c  VelocityZ    0.46304E+04      12   0.74003E-02   0.30122E-04 
c  TurbEner     0.59829E+01      13   0.72590E-04   0.79999E-09 
c  Dissip       0.14775E+01      13   0.29947E-03   0.23941E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.64           54546           26778           27272
v  Velocity[x]              0.293          2.1439         0.90807         0.90985
v  Velocity[y]           -0.36635         0.70257      0.00054871      0.00032572
v  Velocity[z]           -0.41912         0.50632      -0.0012506       -0.001372
v  TurbEner             0.0010831        0.014988       0.0032923       0.0033502
v  Dissip              9.1976e-05        0.030747      0.00045309      0.00039142
v  TurbVisc               0.17514          11.371          4.7189          5.2796
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              599:        0.89336E-01

===============================================================


 INSTANT    0.600000000E+03   TIME STEP NUMBER             600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001901E+04
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 :  0.23749E+00 0.13255E+01
   Friction velocity        uet   :  0.14207E-01 0.79013E-01
   Friction velocity        uk    :  0.18026E-01 0.38802E-01
   Dimensionless distance   yplus :  0.44264E+03 0.95189E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68293E+01      58   0.15973E-02   0.22404E-01 
c  VelocityX    0.46304E+04      12   0.72496E-02   0.41328E-03 
c  VelocityY    0.46304E+04      12   0.72496E-02   0.28568E-04 
c  VelocityZ    0.46304E+04      12   0.72496E-02   0.98619E-04 
c  TurbEner     0.59835E+01      13   0.71529E-04   0.12284E-08 
c  Dissip       0.15046E+01      15   0.86184E-03   0.15669E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -166.9           54523           26778           27273
v  Velocity[x]             0.2926          2.1809         0.90806         0.90984
v  Velocity[y]           -0.38303          0.6922      0.00055909      0.00033761
v  Velocity[z]           -0.42029         0.51036       -0.001238      -0.0013627
v  TurbEner             0.0010767        0.015077       0.0032921       0.0033502
v  Dissip              9.2015e-05        0.031217      0.00045325      0.00039155
v  TurbVisc               0.17544          11.349          4.7187          5.2794
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              600:        0.89879E-01

===============================================================


 INSTANT    0.601000000E+03   TIME STEP NUMBER             601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999190E+04
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 :  0.23771E+00 0.12174E+01
   Friction velocity        uet   :  0.14221E-01 0.72570E-01
   Friction velocity        uk    :  0.17972E-01 0.38637E-01
   Dimensionless distance   yplus :  0.44176E+03 0.95266E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59911E+01      57   0.12554E-02   0.19645E-01 
c  VelocityX    0.46303E+04      12   0.67455E-02   0.33614E-03 
c  VelocityY    0.46303E+04      12   0.67455E-02   0.36475E-04 
c  VelocityZ    0.46303E+04      12   0.67455E-02   0.51197E-04 
c  TurbEner     0.59835E+01      13   0.79260E-04   0.12541E-08 
c  Dissip       0.15353E+01      15   0.10135E-02   0.23167E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.28           54528           26778           27272
v  Velocity[x]            0.29279          2.1986         0.90804         0.90982
v  Velocity[y]           -0.36765         0.70072        0.000553      0.00033083
v  Velocity[z]           -0.42204         0.50424      -0.0012524      -0.0013717
v  TurbEner             0.0010765        0.015208        0.003292       0.0033501
v  Dissip              9.1994e-05         0.03173      0.00045347       0.0003917
v  TurbVisc               0.17471           11.35          4.7184          5.2792
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              601:        0.89709E-01

===============================================================


 INSTANT    0.602000000E+03   TIME STEP NUMBER             602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001364E+04
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 :  0.23782E+00 0.13240E+01
   Friction velocity        uet   :  0.14227E-01 0.78920E-01
   Friction velocity        uk    :  0.17971E-01 0.38704E-01
   Dimensionless distance   yplus :  0.44099E+03 0.95286E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62956E+01      56   0.14306E-02   0.20631E-01 
c  VelocityX    0.46302E+04      12   0.68358E-02   0.40083E-03 
c  VelocityY    0.46302E+04      12   0.68358E-02   0.22007E-04 
c  VelocityZ    0.46302E+04      12   0.68358E-02   0.30904E-04 
c  TurbEner     0.59836E+01      13   0.11712E-03   0.12938E-08 
c  Dissip       0.15538E+01      16   0.22192E-02   0.57241E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.71           54524           26777           27271
v  Velocity[x]            0.29271          2.0389         0.90806         0.90984
v  Velocity[y]           -0.38256         0.69387      0.00054691      0.00032718
v  Velocity[z]           -0.42044         0.51169       -0.001245      -0.0013684
v  TurbEner             0.0010741        0.015758       0.0032918       0.0033499
v  Dissip               9.202e-05        0.033502      0.00045373      0.00039191
v  TurbVisc               0.17418          11.305          4.7182          5.2789
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              602:        0.90106E-01

===============================================================


 INSTANT    0.603000000E+03   TIME STEP NUMBER             603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002231E+04
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 :  0.23773E+00 0.12167E+01
   Friction velocity        uet   :  0.14221E-01 0.72531E-01
   Friction velocity        uk    :  0.17951E-01 0.38779E-01
   Dimensionless distance   yplus :  0.44097E+03 0.95356E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57472E+01      59   0.12850E-02   0.18857E-01 
c  VelocityX    0.46302E+04      12   0.63018E-02   0.35182E-03 
c  VelocityY    0.46302E+04      12   0.63018E-02   0.22410E-04 
c  VelocityZ    0.46302E+04      12   0.63018E-02   0.38743E-04 
c  TurbEner     0.59818E+01      13   0.14980E-03   0.20403E-08 
c  Dissip       0.15247E+01      16   0.20054E-02   0.60301E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.63           54506           26777           27271
v  Velocity[x]            0.29276          2.1053         0.90806         0.90984
v  Velocity[y]           -0.36629         0.70238      0.00054487      0.00032376
v  Velocity[z]           -0.42083         0.50637      -0.0012495        -0.00137
v  TurbEner             0.0010678        0.015099       0.0032914       0.0033497
v  Dissip              9.2034e-05        0.032172      0.00045354      0.00039179
v  TurbVisc               0.17402          11.302          4.7178          5.2786
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              603:        0.90769E-01

===============================================================


 INSTANT    0.604000000E+03   TIME STEP NUMBER             604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999624E+04
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 :  0.23770E+00 0.13239E+01
   Friction velocity        uet   :  0.14219E-01 0.78915E-01
   Friction velocity        uk    :  0.17898E-01 0.38831E-01
   Dimensionless distance   yplus :  0.44015E+03 0.95391E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64223E+01      58   0.12920E-02   0.21055E-01 
c  VelocityX    0.46302E+04      12   0.72141E-02   0.35028E-03 
c  VelocityY    0.46302E+04      12   0.72141E-02   0.39015E-04 
c  VelocityZ    0.46302E+04      12   0.72141E-02   0.11366E-03 
c  TurbEner     0.59813E+01      13   0.67422E-04   0.11077E-08 
c  Dissip       0.15315E+01      14   0.28034E-03   0.23234E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.96           54526           26777           27272
v  Velocity[x]            0.29276          2.1548         0.90804         0.90982
v  Velocity[y]           -0.38246         0.69444      0.00055842       0.0003345
v  Velocity[z]           -0.42267         0.51102      -0.0012391      -0.0013644
v  TurbEner              0.001065        0.015026       0.0032911       0.0033494
v  Dissip              9.2094e-05        0.032056      0.00045347      0.00039174
v  TurbVisc               0.17328          11.341          4.7174          5.2782
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              604:        0.89716E-01

===============================================================


 INSTANT    0.605000000E+03   TIME STEP NUMBER             605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998720E+04
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 :  0.23758E+00 0.12170E+01
   Friction velocity        uet   :  0.14212E-01 0.72551E-01
   Friction velocity        uk    :  0.17874E-01 0.38820E-01
   Dimensionless distance   yplus :  0.43873E+03 0.95358E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69132E+01      60   0.14478E-02   0.22662E-01 
c  VelocityX    0.46301E+04      12   0.66128E-02   0.31111E-03 
c  VelocityY    0.46301E+04      12   0.66128E-02   0.61584E-04 
c  VelocityZ    0.46301E+04      12   0.66128E-02   0.59963E-04 
c  TurbEner     0.59814E+01      13   0.84788E-04   0.12782E-08 
c  Dissip       0.15500E+01      15   0.94448E-03   0.23364E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.06           54533           26777           27271
v  Velocity[x]            0.29306          2.1798         0.90804         0.90983
v  Velocity[y]             -0.368         0.70118      0.00054631      0.00032313
v  Velocity[z]           -0.41886         0.50397      -0.0012531      -0.0013739
v  TurbEner             0.0010625        0.015117       0.0032908       0.0033492
v  Dissip              9.2115e-05         0.03223      0.00045362      0.00039184
v  TurbVisc               0.17235          11.331          4.7171          5.2779
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              605:        0.90145E-01

===============================================================


 INSTANT    0.606000000E+03   TIME STEP NUMBER             606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000394E+04
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 :  0.23759E+00 0.13259E+01
   Friction velocity        uet   :  0.14212E-01 0.79026E-01
   Friction velocity        uk    :  0.17853E-01 0.38801E-01
   Dimensionless distance   yplus :  0.43885E+03 0.95404E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70515E+01      59   0.16370E-02   0.23128E-01 
c  VelocityX    0.46301E+04      12   0.70897E-02   0.35490E-03 
c  VelocityY    0.46301E+04      12   0.70897E-02   0.44809E-04 
c  VelocityZ    0.46301E+04      12   0.70897E-02   0.29520E-04 
c  TurbEner     0.59817E+01      13   0.10820E-03   0.99607E-09 
c  Dissip       0.15616E+01      15   0.18300E-02   0.36517E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.63           54543           26778           27272
v  Velocity[x]            0.29222          2.0312         0.90804         0.90982
v  Velocity[y]           -0.38273         0.69443      0.00054157      0.00032092
v  Velocity[z]           -0.42024         0.51153      -0.0012524       -0.001375
v  TurbEner             0.0010535        0.015619       0.0032905        0.003349
v  Dissip              9.2128e-05        0.033678      0.00045377      0.00039196
v  TurbVisc               0.17223          11.333          4.7168          5.2775
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              606:        0.89919E-01

===============================================================


 INSTANT    0.607000000E+03   TIME STEP NUMBER             607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998723E+04
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 :  0.23745E+00 0.12134E+01
   Friction velocity        uet   :  0.14204E-01 0.72327E-01
   Friction velocity        uk    :  0.17778E-01 0.38663E-01
   Dimensionless distance   yplus :  0.43736E+03 0.95402E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67359E+01      61   0.13102E-02   0.22079E-01 
c  VelocityX    0.46300E+04      12   0.71276E-02   0.36940E-03 
c  VelocityY    0.46300E+04      12   0.71276E-02   0.28152E-04 
c  VelocityZ    0.46300E+04      12   0.71276E-02   0.40200E-04 
c  TurbEner     0.59802E+01      13   0.13315E-03   0.16052E-08 
c  Dissip       0.15295E+01      16   0.21028E-02   0.62509E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.58           54552           26777           27271
v  Velocity[x]            0.29293          2.0929         0.90805         0.90983
v  Velocity[y]           -0.36676         0.70241      0.00053716      0.00031557
v  Velocity[z]           -0.41996         0.50589      -0.0012565      -0.0013756
v  TurbEner             0.0010509         0.01504         0.00329       0.0033486
v  Dissip              9.2106e-05        0.032263      0.00045351      0.00039178
v  TurbVisc               0.17114          11.366          4.7164          5.2772
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              607:        0.90179E-01

===============================================================


 INSTANT    0.608000000E+03   TIME STEP NUMBER             608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001324E+04
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 :  0.23811E+00 0.13248E+01
   Friction velocity        uet   :  0.14242E-01 0.78966E-01
   Friction velocity        uk    :  0.17756E-01 0.38744E-01
   Dimensionless distance   yplus :  0.43604E+03 0.95351E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64348E+01      59   0.14517E-02   0.21074E-01 
c  VelocityX    0.46300E+04      12   0.74562E-02   0.35616E-03 
c  VelocityY    0.46300E+04      12   0.74562E-02   0.30688E-04 
c  VelocityZ    0.46300E+04      12   0.74562E-02   0.10049E-03 
c  TurbEner     0.59807E+01      13   0.60215E-04   0.77395E-09 
c  Dissip       0.15309E+01      13   0.35052E-03   0.21310E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.65           54540           26776           27271
v  Velocity[x]            0.29317          2.1472         0.90807         0.90985
v  Velocity[y]            -0.3825         0.69223      0.00055095      0.00033016
v  Velocity[z]           -0.42094          0.5109      -0.0012452      -0.0013684
v  TurbEner             0.0010464        0.014983       0.0032899       0.0033485
v  Dissip              9.2095e-05        0.032058      0.00045349      0.00039177
v  TurbVisc                0.1703          11.347           4.716          5.2768
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              608:        0.90069E-01

===============================================================


 INSTANT    0.609000000E+03   TIME STEP NUMBER             609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000688E+04
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 :  0.23768E+00 0.12172E+01
   Friction velocity        uet   :  0.14216E-01 0.72552E-01
   Friction velocity        uk    :  0.17718E-01 0.38828E-01
   Dimensionless distance   yplus :  0.43548E+03 0.95346E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63963E+01      65   0.14567E-02   0.20978E-01 
c  VelocityX    0.46301E+04      13   0.70198E-02   0.43770E-03 
c  VelocityY    0.46301E+04      13   0.70198E-02   0.31928E-04 
c  VelocityZ    0.46301E+04      13   0.70198E-02   0.54060E-04 
c  TurbEner     0.59814E+01      13   0.77182E-04   0.12794E-08 
c  Dissip       0.15468E+01      15   0.69814E-03   0.12709E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.61           54514           26776           27270
v  Velocity[x]             0.2925          2.1782         0.90808         0.90985
v  Velocity[y]           -0.36767         0.70037      0.00054846      0.00032616
v  Velocity[z]           -0.42177         0.50438      -0.0012628      -0.0013811
v  TurbEner              0.001039        0.015049       0.0032898       0.0033485
v  Dissip              9.2048e-05        0.032194       0.0004536      0.00039186
v  TurbVisc               0.16987          11.338          4.7157          5.2765
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              609:        0.92301E-01

===============================================================


 INSTANT    0.610000000E+03   TIME STEP NUMBER             610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000683E+04
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 :  0.23746E+00 0.13240E+01
   Friction velocity        uet   :  0.14203E-01 0.78920E-01
   Friction velocity        uk    :  0.17655E-01 0.38836E-01
   Dimensionless distance   yplus :  0.43438E+03 0.95319E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63807E+01      55   0.13212E-02   0.20921E-01 
c  VelocityX    0.46300E+04      12   0.68385E-02   0.33115E-03 
c  VelocityY    0.46300E+04      12   0.68385E-02   0.44270E-04 
c  VelocityZ    0.46300E+04      12   0.68385E-02   0.33133E-04 
c  TurbEner     0.59815E+01      13   0.74917E-04   0.10722E-08 
c  Dissip       0.15710E+01      15   0.77720E-03   0.11809E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.32           54524           26776           27270
v  Velocity[x]            0.29268          2.2073         0.90804         0.90982
v  Velocity[y]           -0.38239          0.6955      0.00054921       0.0003312
v  Velocity[z]           -0.41968         0.51191      -0.0012473      -0.0013665
v  TurbEner              0.001036        0.015208       0.0032896       0.0033483
v  Dissip              9.2052e-05        0.032654      0.00045374      0.00039195
v  TurbVisc               0.16901          11.372          4.7154          5.2763
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              610:        0.89159E-01

===============================================================


 INSTANT    0.611000000E+03   TIME STEP NUMBER             611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999616E+04
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 :  0.23765E+00 0.12135E+01
   Friction velocity        uet   :  0.14214E-01 0.72341E-01
   Friction velocity        uk    :  0.17629E-01 0.38806E-01
   Dimensionless distance   yplus :  0.43293E+03 0.95256E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70495E+01      65   0.15571E-02   0.23111E-01 
c  VelocityX    0.46298E+04      12   0.69572E-02   0.39571E-03 
c  VelocityY    0.46298E+04      12   0.69572E-02   0.53863E-04 
c  VelocityZ    0.46298E+04      12   0.69572E-02   0.46381E-04 
c  TurbEner     0.59822E+01      14   0.13513E-03   0.18606E-08 
c  Dissip       0.15864E+01      16   0.21412E-02   0.51394E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.28           54532           26776           27270
v  Velocity[x]            0.29326          2.0246         0.90805         0.90983
v  Velocity[y]           -0.36611         0.70409      0.00054001      0.00031727
v  Velocity[z]           -0.42031         0.50649      -0.0012623       -0.001382
v  TurbEner              0.001034         0.01584       0.0032896       0.0033483
v  Dissip              9.2087e-05        0.034362      0.00045396      0.00039212
v  TurbVisc               0.16818          11.354          4.7151           5.276
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              611:        0.91409E-01

===============================================================


 INSTANT    0.612000000E+03   TIME STEP NUMBER             612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999039E+04
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 :  0.23792E+00 0.13251E+01
   Friction velocity        uet   :  0.14231E-01 0.78988E-01
   Friction velocity        uk    :  0.17613E-01 0.38740E-01
   Dimensionless distance   yplus :  0.43309E+03 0.95233E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66912E+01      65   0.13003E-02   0.21938E-01 
c  VelocityX    0.46299E+04      13   0.66241E-02   0.38241E-03 
c  VelocityY    0.46299E+04      13   0.66241E-02   0.46116E-04 
c  VelocityZ    0.46299E+04      13   0.66241E-02   0.11163E-03 
c  TurbEner     0.59809E+01      14   0.13528E-03   0.19136E-08 
c  Dissip       0.15522E+01      16   0.22302E-02   0.74571E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.87           54542           26776           27271
v  Velocity[x]            0.29292          2.1072         0.90804         0.90982
v  Velocity[y]           -0.38231         0.69216       0.0005492      0.00032623
v  Velocity[z]           -0.41854         0.51104      -0.0012461      -0.0013679
v  TurbEner             0.0010261        0.015262       0.0032892        0.003348
v  Dissip              9.2125e-05          0.0329      0.00045371      0.00039196
v  TurbVisc               0.16815          11.361          4.7148          5.2757
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              612:        0.92164E-01

===============================================================


 INSTANT    0.613000000E+03   TIME STEP NUMBER             613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998478E+04
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 :  0.23770E+00 0.12181E+01
   Friction velocity        uet   :  0.14218E-01 0.72600E-01
   Friction velocity        uk    :  0.17545E-01 0.38679E-01
   Dimensionless distance   yplus :  0.43177E+03 0.95211E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61189E+01      57   0.11857E-02   0.20064E-01 
c  VelocityX    0.46299E+04      12   0.67667E-02   0.29095E-03 
c  VelocityY    0.46299E+04      12   0.67667E-02   0.41934E-04 
c  VelocityZ    0.46299E+04      12   0.67667E-02   0.51029E-04 
c  TurbEner     0.59809E+01      12   0.58782E-04   0.62951E-09 
c  Dissip       0.15519E+01      14   0.51116E-03   0.38896E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.18           54550           26777           27271
v  Velocity[x]            0.29259          2.1483         0.90805         0.90983
v  Velocity[y]           -0.36791         0.70095      0.00054536      0.00032009
v  Velocity[z]           -0.41847         0.50398      -0.0012566      -0.0013765
v  TurbEner             0.0010253        0.015168        0.003289       0.0033479
v  Dissip              9.2113e-05        0.032579      0.00045369      0.00039194
v  TurbVisc               0.16704          11.337          4.7144          5.2753
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              613:        0.89548E-01

===============================================================


 INSTANT    0.614000000E+03   TIME STEP NUMBER             614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998823E+04
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 :  0.23766E+00 0.13242E+01
   Friction velocity        uet   :  0.14216E-01 0.78923E-01
   Friction velocity        uk    :  0.17538E-01 0.38737E-01
   Dimensionless distance   yplus :  0.43078E+03 0.95219E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65791E+01      60   0.15073E-02   0.21556E-01 
c  VelocityX    0.46299E+04      12   0.71590E-02   0.35699E-03 
c  VelocityY    0.46299E+04      12   0.71590E-02   0.31343E-04 
c  VelocityZ    0.46299E+04      12   0.71590E-02   0.31581E-04 
c  TurbEner     0.59820E+01      13   0.65321E-04   0.69438E-09 
c  Dissip       0.15727E+01      15   0.69888E-03   0.12315E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.82           54541           26777           27271
v  Velocity[x]            0.29272          2.1924         0.90806         0.90984
v  Velocity[y]           -0.38266          0.6946      0.00054536      0.00032583
v  Velocity[z]           -0.41961         0.51155      -0.0012391      -0.0013604
v  TurbEner              0.001023        0.015216       0.0032889       0.0033478
v  Dissip              9.2147e-05        0.032753      0.00045384      0.00039204
v  TurbVisc               0.16661          11.334          4.7141           5.275
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              614:        0.89964E-01

===============================================================


 INSTANT    0.615000000E+03   TIME STEP NUMBER             615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999979E+04
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 :  0.23805E+00 0.12176E+01
   Friction velocity        uet   :  0.14240E-01 0.72581E-01
   Friction velocity        uk    :  0.17518E-01 0.38777E-01
   Dimensionless distance   yplus :  0.43066E+03 0.95205E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60247E+01      66   0.16256E-02   0.19768E-01 
c  VelocityX    0.46298E+04      12   0.64497E-02   0.41064E-03 
c  VelocityY    0.46298E+04      12   0.64497E-02   0.25373E-04 
c  VelocityZ    0.46298E+04      12   0.64497E-02   0.51505E-04 
c  TurbEner     0.59819E+01      13   0.11422E-03   0.15012E-08 
c  Dissip       0.15803E+01      16   0.18219E-02   0.37240E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.87           54516           26777           27271
v  Velocity[x]            0.29285          2.0218         0.90806         0.90983
v  Velocity[y]           -0.36672         0.70277      0.00054668      0.00032471
v  Velocity[z]              -0.42         0.50586      -0.0012582      -0.0013777
v  TurbEner             0.0010174        0.015728       0.0032888       0.0033478
v  Dissip              9.2136e-05        0.034192      0.00045402      0.00039219
v  TurbVisc               0.16647          11.364          4.7138          5.2747
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              615:        0.92038E-01

===============================================================


 INSTANT    0.616000000E+03   TIME STEP NUMBER             616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999973E+04
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 :  0.23809E+00 0.13236E+01
   Friction velocity        uet   :  0.14242E-01 0.78888E-01
   Friction velocity        uk    :  0.17470E-01 0.38777E-01
   Dimensionless distance   yplus :  0.42978E+03 0.95163E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57808E+01      54   0.12847E-02   0.18956E-01 
c  VelocityX    0.46298E+04      12   0.64686E-02   0.29420E-03 
c  VelocityY    0.46298E+04      12   0.64686E-02   0.29755E-04 
c  VelocityZ    0.46298E+04      12   0.64686E-02   0.10885E-03 
c  TurbEner     0.59795E+01      14   0.14122E-03   0.23138E-08 
c  Dissip       0.15412E+01      17   0.23453E-02   0.83554E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.08           54524           26777           27271
v  Velocity[x]            0.29258          2.0942         0.90803         0.90981
v  Velocity[y]           -0.38244          0.6954      0.00055033      0.00033137
v  Velocity[z]           -0.42087         0.51093      -0.0012435      -0.0013679
v  TurbEner             0.0010164        0.015138       0.0032884       0.0033475
v  Dissip              9.2079e-05        0.032698       0.0004537      0.00039198
v  TurbVisc                0.1657          11.344          4.7135          5.2744
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              616:        0.89669E-01

===============================================================


 INSTANT    0.617000000E+03   TIME STEP NUMBER             617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000897E+04
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 :  0.23790E+00 0.12172E+01
   Friction velocity        uet   :  0.14232E-01 0.72559E-01
   Friction velocity        uk    :  0.17462E-01 0.38705E-01
   Dimensionless distance   yplus :  0.42867E+03 0.95178E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60980E+01      57   0.12854E-02   0.19982E-01 
c  VelocityX    0.46298E+04      12   0.66882E-02   0.36822E-03 
c  VelocityY    0.46298E+04      12   0.66882E-02   0.26662E-04 
c  VelocityZ    0.46298E+04      12   0.66882E-02   0.48505E-04 
c  TurbEner     0.59793E+01      13   0.62711E-04   0.70122E-09 
c  Dissip       0.15424E+01      14   0.53687E-03   0.41624E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.01           54532           26776           27270
v  Velocity[x]            0.29308          2.1453         0.90805         0.90982
v  Velocity[y]           -0.36764          0.7016       0.0005476      0.00032513
v  Velocity[z]           -0.42121         0.50438      -0.0012568      -0.0013767
v  TurbEner             0.0010166        0.015008        0.003288       0.0033471
v  Dissip              9.2084e-05        0.032366       0.0004536       0.0003919
v  TurbVisc               0.16518          11.341          4.7131          5.2741
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              617:        0.90072E-01

===============================================================


 INSTANT    0.618000000E+03   TIME STEP NUMBER             618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002644E+04
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 :  0.23781E+00 0.13259E+01
   Friction velocity        uet   :  0.14226E-01 0.79027E-01
   Friction velocity        uk    :  0.17464E-01 0.38741E-01
   Dimensionless distance   yplus :  0.42916E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56701E+01      55   0.11817E-02   0.18582E-01 
c  VelocityX    0.46299E+04      13   0.66336E-02   0.30901E-03 
c  VelocityY    0.46299E+04      13   0.66336E-02   0.22877E-04 
c  VelocityZ    0.46299E+04      13   0.66336E-02   0.31435E-04 
c  TurbEner     0.59798E+01      12   0.65878E-04   0.67661E-09 
c  Dissip       0.15605E+01      14   0.62843E-03   0.97454E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.13           54540           26775           27269
v  Velocity[x]            0.29266          2.1847         0.90806         0.90984
v  Velocity[y]           -0.38235         0.69464      0.00053752      0.00031829
v  Velocity[z]           -0.42137         0.51177      -0.0012475       -0.001369
v  TurbEner             0.0010116        0.015036       0.0032876       0.0033469
v  Dissip              9.2059e-05        0.032505      0.00045361       0.0003919
v  TurbVisc                0.1654          11.315          4.7128          5.2738
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              618:        0.90033E-01

===============================================================


 INSTANT    0.619000000E+03   TIME STEP NUMBER             619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001499E+04
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 :  0.23799E+00 0.12136E+01
   Friction velocity        uet   :  0.14236E-01 0.72338E-01
   Friction velocity        uk    :  0.17421E-01 0.38683E-01
   Dimensionless distance   yplus :  0.42841E+03 0.95179E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61033E+01      59   0.14376E-02   0.20018E-01 
c  VelocityX    0.46298E+04      12   0.68720E-02   0.32929E-03 
c  VelocityY    0.46298E+04      12   0.68720E-02   0.33975E-04 
c  VelocityZ    0.46298E+04      12   0.68720E-02   0.39194E-04 
c  TurbEner     0.59798E+01      13   0.10516E-03   0.99176E-09 
c  Dissip       0.15681E+01      15   0.17901E-02   0.34536E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.33           54548           26775           27269
v  Velocity[x]            0.29272          2.0134         0.90806         0.90983
v  Velocity[y]           -0.36619          0.7023      0.00054286      0.00032025
v  Velocity[z]           -0.42064         0.50635      -0.0012638      -0.0013841
v  TurbEner             0.0010133        0.015534       0.0032875       0.0033468
v  Dissip              9.2035e-05         0.03391      0.00045371      0.00039197
v  TurbVisc               0.16476          11.322          4.7125          5.2736
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              619:        0.89895E-01

===============================================================


 INSTANT    0.620000000E+03   TIME STEP NUMBER             620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000622E+04
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 :  0.23760E+00 0.13250E+01
   Friction velocity        uet   :  0.14213E-01 0.78979E-01
   Friction velocity        uk    :  0.17436E-01 0.38712E-01
   Dimensionless distance   yplus :  0.42798E+03 0.95178E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66894E+01      67   0.16344E-02   0.21913E-01 
c  VelocityX    0.46297E+04      12   0.70216E-02   0.40051E-03 
c  VelocityY    0.46297E+04      12   0.70216E-02   0.52449E-04 
c  VelocityZ    0.46297E+04      12   0.70216E-02   0.11723E-03 
c  TurbEner     0.59788E+01      14   0.14321E-03   0.21682E-08 
c  Dissip       0.15341E+01      17   0.23923E-02   0.81241E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.57           54539           26775           27269
v  Velocity[x]            0.29301          2.0976         0.90804         0.90982
v  Velocity[y]           -0.38242         0.69171      0.00055519      0.00033529
v  Velocity[z]           -0.41959         0.51094      -0.0012364      -0.0013589
v  TurbEner             0.0010134        0.014919       0.0032872       0.0033466
v  Dissip              9.2033e-05        0.032347      0.00045339      0.00039176
v  TurbVisc                0.1646          11.361          4.7123          5.2734
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              620:        0.91102E-01

===============================================================


 INSTANT    0.621000000E+03   TIME STEP NUMBER             621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000257E+04
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 :  0.23768E+00 0.12169E+01
   Friction velocity        uet   :  0.14218E-01 0.72539E-01
   Friction velocity        uk    :  0.17436E-01 0.38745E-01
   Dimensionless distance   yplus :  0.42842E+03 0.95226E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63319E+01      67   0.15102E-02   0.20776E-01 
c  VelocityX    0.46298E+04      13   0.68253E-02   0.41276E-03 
c  VelocityY    0.46298E+04      13   0.68253E-02   0.31240E-04 
c  VelocityZ    0.46298E+04      13   0.68253E-02   0.58617E-04 
c  TurbEner     0.59786E+01      13   0.73679E-04   0.99015E-09 
c  Dissip       0.15274E+01      14   0.76611E-03   0.73940E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.29           54515           26776           27270
v  Velocity[x]            0.29279          2.1455         0.90806         0.90984
v  Velocity[y]            -0.3679          0.6995      0.00055606      0.00033379
v  Velocity[z]           -0.42061         0.50401      -0.0012456      -0.0013645
v  TurbEner             0.0010104         0.01476        0.003287       0.0033464
v  Dissip              9.2081e-05        0.031829      0.00045318      0.00039161
v  TurbVisc               0.16481          11.344          4.7121          5.2733
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              621:        0.92809E-01

===============================================================


 INSTANT    0.622000000E+03   TIME STEP NUMBER             622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998995E+04
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 :  0.23767E+00 0.13240E+01
   Friction velocity        uet   :  0.14217E-01 0.78918E-01
   Friction velocity        uk    :  0.17411E-01 0.38778E-01
   Dimensionless distance   yplus :  0.42817E+03 0.95231E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63646E+01      56   0.12293E-02   0.20850E-01 
c  VelocityX    0.46298E+04      12   0.73908E-02   0.37210E-03 
c  VelocityY    0.46298E+04      12   0.73908E-02   0.33862E-04 
c  VelocityZ    0.46298E+04      12   0.73908E-02   0.30542E-04 
c  TurbEner     0.59784E+01      13   0.80160E-04   0.10908E-08 
c  Dissip       0.15416E+01      14   0.54618E-03   0.77338E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.75           54522           26776           27270
v  Velocity[x]            0.29258          2.1868         0.90805         0.90983
v  Velocity[y]           -0.38299         0.69241      0.00055369      0.00033469
v  Velocity[z]           -0.42162         0.51129      -0.0012418      -0.0013644
v  TurbEner             0.0010112         0.01481       0.0032866       0.0033462
v  Dissip               9.216e-05        0.031888      0.00045312      0.00039156
v  TurbVisc               0.16443          11.346           4.712          5.2731
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              622:        0.89801E-01

===============================================================


 INSTANT    0.623000000E+03   TIME STEP NUMBER             623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000089E+04
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 :  0.23743E+00 0.12162E+01
   Friction velocity        uet   :  0.14202E-01 0.72499E-01
   Friction velocity        uk    :  0.17417E-01 0.38743E-01
   Dimensionless distance   yplus :  0.42744E+03 0.95235E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69255E+01      64   0.15264E-02   0.22699E-01 
c  VelocityX    0.46297E+04      12   0.64219E-02   0.43682E-03 
c  VelocityY    0.46297E+04      12   0.64219E-02   0.47473E-04 
c  VelocityZ    0.46297E+04      12   0.64219E-02   0.37439E-04 
c  TurbEner     0.59784E+01      13   0.11875E-03   0.14368E-08 
c  Dissip       0.15484E+01      16   0.18047E-02   0.34434E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.75           54531           26775           27269
v  Velocity[x]            0.29272          2.0124         0.90805         0.90982
v  Velocity[y]           -0.36804         0.70053      0.00054849      0.00032601
v  Velocity[z]           -0.41857           0.507      -0.0012586      -0.0013763
v  TurbEner             0.0010128         0.01537       0.0032865        0.003346
v  Dissip              9.2183e-05        0.033291      0.00045317       0.0003916
v  TurbVisc               0.16414          11.324          4.7118           5.273
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              623:        0.91432E-01

===============================================================


 INSTANT    0.624000000E+03   TIME STEP NUMBER             624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000698E+04
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 :  0.23774E+00 0.13235E+01
   Friction velocity        uet   :  0.14220E-01 0.78890E-01
   Friction velocity        uk    :  0.17431E-01 0.38749E-01
   Dimensionless distance   yplus :  0.42830E+03 0.95282E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58096E+01      56   0.12742E-02   0.19040E-01 
c  VelocityX    0.46298E+04      12   0.72050E-02   0.27508E-03 
c  VelocityY    0.46298E+04      12   0.72050E-02   0.25326E-04 
c  VelocityZ    0.46298E+04      12   0.72050E-02   0.55487E-04 
c  TurbEner     0.59774E+01      14   0.14443E-03   0.21551E-08 
c  Dissip       0.15066E+01      17   0.24691E-02   0.88897E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.24           54539           26775           27269
v  Velocity[x]            0.29276          2.0938         0.90805         0.90983
v  Velocity[y]           -0.38267         0.69327      0.00054606      0.00032568
v  Velocity[z]           -0.42048         0.51372      -0.0012533      -0.0013736
v  TurbEner             0.0010077        0.014788       0.0032861       0.0033458
v  Dissip              9.2144e-05        0.031744      0.00045275      0.00039131
v  TurbVisc               0.16457          11.317          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              624:        0.89776E-01

===============================================================


 INSTANT    0.625000000E+03   TIME STEP NUMBER             625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999106E+04
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 :  0.23782E+00 0.12224E+01
   Friction velocity        uet   :  0.14225E-01 0.72455E-01
   Friction velocity        uk    :  0.17387E-01 0.38661E-01
   Dimensionless distance   yplus :  0.42761E+03 0.95224E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59741E+01      56   0.12764E-02   0.19584E-01 
c  VelocityX    0.46298E+04      12   0.71378E-02   0.34424E-03 
c  VelocityY    0.46298E+04      12   0.71378E-02   0.27816E-04 
c  VelocityZ    0.46298E+04      12   0.71378E-02   0.42911E-04 
c  TurbEner     0.59776E+01      13   0.72932E-04   0.83884E-09 
c  Dissip       0.15054E+01      14   0.67555E-03   0.53009E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -179.29           54547           26775           27269
v  Velocity[x]            0.29285           2.144         0.90807         0.90984
v  Velocity[y]           -0.36653         0.70115      0.00054866      0.00032763
v  Velocity[z]           -0.41943          0.5079       -0.001265      -0.0013806
v  TurbEner             0.0010088        0.014672       0.0032861       0.0033457
v  Dissip              9.2149e-05        0.031289      0.00045262      0.00039122
v  TurbVisc               0.16393           11.33          4.7115          5.2727
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              625:        0.89292E-01

===============================================================


 INSTANT    0.626000000E+03   TIME STEP NUMBER             626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000575E+04
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 :  0.23795E+00 0.13251E+01
   Friction velocity        uet   :  0.14232E-01 0.78987E-01
   Friction velocity        uk    :  0.17396E-01 0.38680E-01
   Dimensionless distance   yplus :  0.42710E+03 0.95219E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68190E+01      60   0.16195E-02   0.22335E-01 
c  VelocityX    0.46298E+04      12   0.75398E-02   0.38197E-03 
c  VelocityY    0.46298E+04      12   0.75398E-02   0.36680E-04 
c  VelocityZ    0.46298E+04      12   0.75398E-02   0.96114E-04 
c  TurbEner     0.59786E+01      12   0.62566E-04   0.68490E-09 
c  Dissip       0.15197E+01      14   0.60084E-03   0.88830E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.32           54539           26775           27269
v  Velocity[x]            0.29273          2.1873         0.90807         0.90985
v  Velocity[y]           -0.38274         0.69444      0.00054559      0.00032933
v  Velocity[z]           -0.42014         0.51196      -0.0012371      -0.0013583
v  TurbEner             0.0010073        0.014754       0.0032861       0.0033457
v  Dissip              9.2088e-05         0.03136      0.00045265      0.00039124
v  TurbVisc                0.1638          11.376          4.7114          5.2727
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              626:        0.89772E-01

===============================================================


 INSTANT    0.627000000E+03   TIME STEP NUMBER             627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999833E+04
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 :  0.23777E+00 0.12308E+01
   Friction velocity        uet   :  0.14221E-01 0.72344E-01
   Friction velocity        uk    :  0.17384E-01 0.38736E-01
   Dimensionless distance   yplus :  0.42727E+03 0.95198E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62337E+01      71   0.16030E-02   0.20460E-01 
c  VelocityX    0.46298E+04      13   0.65297E-02   0.45770E-03 
c  VelocityY    0.46298E+04      13   0.65297E-02   0.24072E-04 
c  VelocityZ    0.46298E+04      13   0.65297E-02   0.43891E-04 
c  TurbEner     0.59789E+01      13   0.12759E-03   0.16290E-08 
c  Dissip       0.15308E+01      16   0.20334E-02   0.43682E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.77           54514           26776           27270
v  Velocity[x]            0.29254          2.0223         0.90807         0.90984
v  Velocity[y]           -0.36825         0.70255      0.00054864      0.00032988
v  Velocity[z]            -0.4219         0.50482      -0.0012492      -0.0013665
v  TurbEner             0.0010032        0.015357       0.0032861       0.0033458
v  Dissip              9.2096e-05         0.03294      0.00045275      0.00039133
v  TurbVisc               0.16391           11.36          4.7114          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              627:        0.93482E-01

===============================================================


 INSTANT    0.628000000E+03   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999141E+04
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 :  0.23761E+00 0.13254E+01
   Friction velocity        uet   :  0.14211E-01 0.79007E-01
   Friction velocity        uk    :  0.17348E-01 0.38761E-01
   Dimensionless distance   yplus :  0.42682E+03 0.95175E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54570E+01      53   0.13012E-02   0.17896E-01 
c  VelocityX    0.46297E+04      12   0.63388E-02   0.30923E-03 
c  VelocityY    0.46297E+04      12   0.63388E-02   0.23664E-04 
c  VelocityZ    0.46297E+04      12   0.63388E-02   0.52351E-04 
c  TurbEner     0.59769E+01      14   0.12851E-03   0.20880E-08 
c  Dissip       0.14977E+01      16   0.21010E-02   0.64920E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.15           54523           26776           27270
v  Velocity[x]            0.29275          2.0947         0.90804         0.90981
v  Velocity[y]           -0.38263         0.69257      0.00054603      0.00032631
v  Velocity[z]           -0.41967         0.51229      -0.0012453      -0.0013647
v  TurbEner             0.0010029        0.014816       0.0032858       0.0033455
v  Dissip              9.2076e-05        0.031616      0.00045247      0.00039114
v  TurbVisc               0.16348          11.364          4.7113          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              628:        0.89332E-01

===============================================================


 INSTANT    0.629000000E+03   TIME STEP NUMBER             629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998589E+04
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 :  0.23765E+00 0.12170E+01
   Friction velocity        uet   :  0.14213E-01 0.72544E-01
   Friction velocity        uk    :  0.17345E-01 0.38704E-01
   Dimensionless distance   yplus :  0.42597E+03 0.95222E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61013E+01      58   0.12978E-02   0.19989E-01 
c  VelocityX    0.46297E+04      12   0.67377E-02   0.29279E-03 
c  VelocityY    0.46297E+04      12   0.67377E-02   0.28055E-04 
c  VelocityZ    0.46297E+04      12   0.67377E-02   0.47982E-04 
c  TurbEner     0.59768E+01      12   0.59162E-04   0.62617E-09 
c  Dissip       0.14988E+01      14   0.57768E-03   0.41180E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.63           54532           26775           27269
v  Velocity[x]            0.29313          2.1431         0.90805         0.90982
v  Velocity[y]           -0.36622         0.70066      0.00054848       0.0003273
v  Velocity[z]           -0.41965         0.50678      -0.0012563      -0.0013723
v  TurbEner              0.001004        0.014699       0.0032856       0.0033454
v  Dissip              9.2057e-05        0.031241      0.00045237      0.00039106
v  TurbVisc               0.16327           11.34          4.7111          5.2724
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              629:        0.90030E-01

===============================================================


 INSTANT    0.630000000E+03   TIME STEP NUMBER             630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001761E+04
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 :  0.23781E+00 0.13242E+01
   Friction velocity        uet   :  0.14223E-01 0.78931E-01
   Friction velocity        uk    :  0.17355E-01 0.38707E-01
   Dimensionless distance   yplus :  0.42670E+03 0.95267E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.76748E+01      62   0.14968E-02   0.25156E-01 
c  VelocityX    0.46298E+04      13   0.75146E-02   0.35387E-03 
c  VelocityY    0.46298E+04      13   0.75146E-02   0.59494E-04 
c  VelocityZ    0.46298E+04      13   0.75146E-02   0.98725E-04 
c  TurbEner     0.59777E+01      12   0.72203E-04   0.74657E-09 
c  Dissip       0.15189E+01      15   0.66422E-03   0.10761E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.36           54539           26775           27269
v  Velocity[x]            0.29263          2.1901         0.90804         0.90981
v  Velocity[y]           -0.38247         0.69617       0.0005549      0.00033515
v  Velocity[z]           -0.42209         0.51114      -0.0012418       -0.001364
v  TurbEner            0.00099972        0.014789       0.0032855       0.0033453
v  Dissip              9.2054e-05        0.031314      0.00045246      0.00039111
v  TurbVisc               0.16377          11.336          4.7111          5.2724
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              630:        0.91443E-01

===============================================================


 INSTANT    0.631000000E+03   TIME STEP NUMBER             631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999890E+04
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 :  0.23772E+00 0.12135E+01
   Friction velocity        uet   :  0.14217E-01 0.72339E-01
   Friction velocity        uk    :  0.17318E-01 0.38653E-01
   Dimensionless distance   yplus :  0.42606E+03 0.95304E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75338E+01      60   0.15622E-02   0.24701E-01 
c  VelocityX    0.46296E+04      13   0.67952E-02   0.41375E-03 
c  VelocityY    0.46296E+04      13   0.67952E-02   0.72894E-04 
c  VelocityZ    0.46296E+04      13   0.67952E-02   0.55550E-04 
c  TurbEner     0.59779E+01      13   0.13865E-03   0.18994E-08 
c  Dissip       0.15192E+01      16   0.18784E-02   0.37214E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -178.5           54547           26775           27269
v  Velocity[x]            0.29283          2.0048         0.90805         0.90983
v  Velocity[y]           -0.36806          0.7043      0.00054847      0.00032459
v  Velocity[z]           -0.42136         0.50411      -0.0012591       -0.001378
v  TurbEner             0.0010025        0.015475       0.0032855       0.0033453
v  Dissip              9.2018e-05        0.032769      0.00045258       0.0003912
v  TurbVisc               0.16334          11.364          4.7111          5.2724
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              631:        0.91584E-01

===============================================================


 INSTANT    0.632000000E+03   TIME STEP NUMBER             632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999672E+04
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 :  0.23799E+00 0.13252E+01
   Friction velocity        uet   :  0.14233E-01 0.78993E-01
   Friction velocity        uk    :  0.17342E-01 0.38715E-01
   Dimensionless distance   yplus :  0.42578E+03 0.95307E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69518E+01      58   0.15038E-02   0.22784E-01 
c  VelocityX    0.46297E+04      13   0.71145E-02   0.38130E-03 
c  VelocityY    0.46297E+04      13   0.71145E-02   0.44881E-04 
c  VelocityZ    0.46297E+04      13   0.71145E-02   0.33626E-04 
c  TurbEner     0.59774E+01      13   0.13335E-03   0.16317E-08 
c  Dissip       0.14857E+01      16   0.23689E-02   0.70697E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.31           54541           26776           27270
v  Velocity[x]            0.29279          2.1001         0.90806         0.90984
v  Velocity[y]           -0.38287         0.69197      0.00055305      0.00033364
v  Velocity[z]           -0.42049          0.5115      -0.0012512      -0.0013726
v  TurbEner             0.0010038        0.014848       0.0032855       0.0033453
v  Dissip              9.2009e-05        0.031129      0.00045234      0.00039103
v  TurbVisc                0.1634          11.344           4.711          5.2723
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              632:        0.90616E-01

===============================================================


 INSTANT    0.633000000E+03   TIME STEP NUMBER             633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997049E+04
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 :  0.23777E+00 0.12191E+01
   Friction velocity        uet   :  0.14221E-01 0.72570E-01
   Friction velocity        uk    :  0.17354E-01 0.38793E-01
   Dimensionless distance   yplus :  0.42639E+03 0.95280E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75663E+01      59   0.16586E-02   0.24802E-01 
c  VelocityX    0.46298E+04      12   0.74021E-02   0.44384E-03 
c  VelocityY    0.46298E+04      12   0.74021E-02   0.41310E-04 
c  VelocityZ    0.46298E+04      12   0.74021E-02   0.51344E-04 
c  TurbEner     0.59779E+01      13   0.67512E-04   0.12839E-08 
c  Dissip       0.14863E+01      14   0.35933E-03   0.25108E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.52           54515           26777           27271
v  Velocity[x]            0.29276           2.139         0.90808         0.90985
v  Velocity[y]           -0.36809         0.70114      0.00054937      0.00032895
v  Velocity[z]           -0.42263         0.50713      -0.0012588      -0.0013733
v  TurbEner             0.0010017        0.014833       0.0032855       0.0033453
v  Dissip              9.2003e-05        0.030905      0.00045228      0.00039099
v  TurbVisc                0.1638          11.356          4.7111          5.2724
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              633:        0.89983E-01

===============================================================


 INSTANT    0.634000000E+03   TIME STEP NUMBER             634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997889E+04
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 :  0.23748E+00 0.13239E+01
   Friction velocity        uet   :  0.14203E-01 0.78909E-01
   Friction velocity        uk    :  0.17335E-01 0.38800E-01
   Dimensionless distance   yplus :  0.42621E+03 0.95229E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61452E+01      62   0.12596E-02   0.20141E-01 
c  VelocityX    0.46299E+04      12   0.66018E-02   0.41320E-03 
c  VelocityY    0.46299E+04      12   0.66018E-02   0.34121E-04 
c  VelocityZ    0.46299E+04      12   0.66018E-02   0.36684E-04 
c  TurbEner     0.59785E+01      13   0.77836E-04   0.14116E-08 
c  Dissip       0.15069E+01      15   0.70271E-03   0.12111E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.52           54521           26777           27271
v  Velocity[x]            0.29287          2.1825         0.90806         0.90983
v  Velocity[y]           -0.38285         0.69503      0.00055023      0.00033087
v  Velocity[z]           -0.41929          0.5138      -0.0012501       -0.001369
v  TurbEner             0.0010041        0.014947       0.0032857       0.0033454
v  Dissip              9.2012e-05        0.031136      0.00045242      0.00039106
v  TurbVisc               0.16364          11.335          4.7111          5.2724
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              634:        0.90348E-01

===============================================================


 INSTANT    0.635000000E+03   TIME STEP NUMBER             635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000164E+04
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 :  0.23768E+00 0.12173E+01
   Friction velocity        uet   :  0.14215E-01 0.72567E-01
   Friction velocity        uk    :  0.17356E-01 0.38729E-01
   Dimensionless distance   yplus :  0.42575E+03 0.95163E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60978E+01      56   0.15375E-02   0.19985E-01 
c  VelocityX    0.46297E+04      12   0.72639E-02   0.38889E-03 
c  VelocityY    0.46297E+04      12   0.72639E-02   0.31956E-04 
c  VelocityZ    0.46297E+04      12   0.72639E-02   0.43183E-04 
c  TurbEner     0.59787E+01      13   0.12490E-03   0.15494E-08 
c  Dissip       0.15154E+01      16   0.18390E-02   0.37568E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.45           54522           26776           27270
v  Velocity[x]            0.29289          2.0149         0.90806         0.90984
v  Velocity[y]           -0.36665         0.70153      0.00055091      0.00033072
v  Velocity[z]           -0.42001         0.50784        -0.00126      -0.0013787
v  TurbEner             0.0010071        0.015514       0.0032858       0.0033454
v  Dissip              9.1991e-05        0.032569      0.00045258      0.00039117
v  TurbVisc               0.16343          11.338          4.7112          5.2724
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              635:        0.89684E-01

===============================================================


 INSTANT    0.636000000E+03   TIME STEP NUMBER             636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002073E+04
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 :  0.23758E+00 0.13261E+01
   Friction velocity        uet   :  0.14209E-01 0.79045E-01
   Friction velocity        uk    :  0.17382E-01 0.38726E-01
   Dimensionless distance   yplus :  0.42685E+03 0.95106E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63803E+01      59   0.14898E-02   0.20938E-01 
c  VelocityX    0.46298E+04      13   0.67394E-02   0.35776E-03 
c  VelocityY    0.46298E+04      13   0.67394E-02   0.31937E-04 
c  VelocityZ    0.46298E+04      13   0.67394E-02   0.11786E-03 
c  TurbEner     0.59773E+01      14   0.12439E-03   0.18955E-08 
c  Dissip       0.14851E+01      16   0.21004E-02   0.66808E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.14           54518           26777           27271
v  Velocity[x]            0.29263          2.0956         0.90805         0.90983
v  Velocity[y]           -0.38271         0.69514      0.00055479      0.00033502
v  Velocity[z]           -0.42153          0.5121      -0.0012353      -0.0013588
v  TurbEner             0.0010044        0.014993       0.0032856       0.0033453
v  Dissip              9.2056e-05        0.031244      0.00045232      0.00039099
v  TurbVisc               0.16402          11.318          4.7112          5.2724
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              636:        0.90821E-01

===============================================================


 INSTANT    0.637000000E+03   TIME STEP NUMBER             637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998026E+04
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 :  0.23769E+00 0.12142E+01
   Friction velocity        uet   :  0.14215E-01 0.72380E-01
   Friction velocity        uk    :  0.17359E-01 0.38676E-01
   Dimensionless distance   yplus :  0.42662E+03 0.95053E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62621E+01      60   0.13058E-02   0.20528E-01 
c  VelocityX    0.46298E+04      13   0.72619E-02   0.39674E-03 
c  VelocityY    0.46298E+04      13   0.72619E-02   0.26020E-04 
c  VelocityZ    0.46298E+04      13   0.72619E-02   0.48559E-04 
c  TurbEner     0.59765E+01      13   0.65879E-04   0.95357E-09 
c  Dissip       0.14845E+01      14   0.52389E-03   0.45526E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.49           54517           26777           27271
v  Velocity[x]            0.29276          2.1445         0.90806         0.90983
v  Velocity[y]           -0.36797         0.70403      0.00055466      0.00033045
v  Velocity[z]           -0.42091         0.50497       -0.001253      -0.0013726
v  TurbEner              0.001008        0.014889       0.0032854        0.003345
v  Dissip              9.2135e-05        0.030937       0.0004522      0.00039088
v  TurbVisc               0.16376          11.314          4.7111          5.2724
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              637:        0.90227E-01

===============================================================


 INSTANT    0.638000000E+03   TIME STEP NUMBER             638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001156E+04
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 :  0.23798E+00 0.13251E+01
   Friction velocity        uet   :  0.14232E-01 0.78987E-01
   Friction velocity        uk    :  0.17389E-01 0.38729E-01
   Dimensionless distance   yplus :  0.42664E+03 0.95064E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63781E+01      67   0.13958E-02   0.20897E-01 
c  VelocityX    0.46298E+04      13   0.65492E-02   0.39633E-03 
c  VelocityY    0.46298E+04      13   0.65492E-02   0.36989E-04 
c  VelocityZ    0.46298E+04      13   0.65492E-02   0.32738E-04 
c  TurbEner     0.59772E+01      13   0.74758E-04   0.91810E-09 
c  Dissip       0.15072E+01      15   0.69738E-03   0.11856E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.87           54529           26776           27270
v  Velocity[x]            0.29298          2.1868         0.90804         0.90982
v  Velocity[y]           -0.38264         0.69204      0.00055588      0.00033243
v  Velocity[z]           -0.42017         0.51227      -0.0012436       -0.001364
v  TurbEner             0.0010093        0.014965       0.0032853       0.0033449
v  Dissip              9.2155e-05        0.031126      0.00045229      0.00039093
v  TurbVisc               0.16378          11.342           4.711          5.2723
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              638:        0.92520E-01

===============================================================


 INSTANT    0.639000000E+03   TIME STEP NUMBER             639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001599E+04
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 :  0.23774E+00 0.12181E+01
   Friction velocity        uet   :  0.14218E-01 0.72604E-01
   Friction velocity        uk    :  0.17401E-01 0.38753E-01
   Dimensionless distance   yplus :  0.42738E+03 0.95107E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63343E+01      63   0.13892E-02   0.20777E-01 
c  VelocityX    0.46298E+04      12   0.68666E-02   0.36280E-03 
c  VelocityY    0.46298E+04      12   0.68666E-02   0.43573E-04 
c  VelocityZ    0.46298E+04      12   0.68666E-02   0.43494E-04 
c  TurbEner     0.59776E+01      13   0.11794E-03   0.13962E-08 
c  Dissip       0.15174E+01      16   0.18828E-02   0.41016E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.45           54540           26775           27269
v  Velocity[x]            0.29279          2.0114         0.90805         0.90983
v  Velocity[y]           -0.36666         0.70052      0.00055112      0.00032707
v  Velocity[z]           -0.42263         0.50642      -0.0012615      -0.0013806
v  TurbEner             0.0010073        0.015538       0.0032852       0.0033449
v  Dissip              9.2132e-05        0.032585      0.00045236      0.00039098
v  TurbVisc               0.16416          11.324           4.711          5.2723
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              639:        0.91092E-01

===============================================================


 INSTANT    0.640000000E+03   TIME STEP NUMBER             640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000790E+04
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 :  0.23757E+00 0.13241E+01
   Friction velocity        uet   :  0.14208E-01 0.78925E-01
   Friction velocity        uk    :  0.17383E-01 0.38734E-01
   Dimensionless distance   yplus :  0.42734E+03 0.95138E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65598E+01      55   0.13023E-02   0.21506E-01 
c  VelocityX    0.46298E+04      12   0.70383E-02   0.33729E-03 
c  VelocityY    0.46298E+04      12   0.70383E-02   0.41358E-04 
c  VelocityZ    0.46298E+04      12   0.70383E-02   0.11752E-03 
c  TurbEner     0.59766E+01      14   0.13657E-03   0.20905E-08 
c  Dissip       0.14843E+01      17   0.22358E-02   0.75972E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.64           54548           26775           27269
v  Velocity[x]            0.29247          2.0979         0.90804         0.90982
v  Velocity[y]           -0.38228         0.69466      0.00055815      0.00033486
v  Velocity[z]           -0.41916         0.51131      -0.0012388      -0.0013609
v  TurbEner             0.0010091        0.014966       0.0032851       0.0033448
v  Dissip              9.2114e-05        0.031173       0.0004521      0.00039079
v  TurbVisc                 0.164          11.332          4.7111          5.2724
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              640:        0.89344E-01

===============================================================


 INSTANT    0.641000000E+03   TIME STEP NUMBER             641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000041E+04
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 :  0.23760E+00 0.12171E+01
   Friction velocity        uet   :  0.14210E-01 0.72562E-01
   Friction velocity        uk    :  0.17399E-01 0.38718E-01
   Dimensionless distance   yplus :  0.42686E+03 0.95163E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67222E+01      56   0.14600E-02   0.22027E-01 
c  VelocityX    0.46297E+04      13   0.72278E-02   0.36924E-03 
c  VelocityY    0.46297E+04      13   0.72278E-02   0.47810E-04 
c  VelocityZ    0.46297E+04      13   0.72278E-02   0.52007E-04 
c  TurbEner     0.59770E+01      12   0.76677E-04   0.71659E-09 
c  Dissip       0.14848E+01      14   0.48082E-03   0.38455E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.84           54539           26775           27270
v  Velocity[x]            0.29287          2.1436         0.90806         0.90985
v  Velocity[y]           -0.36697         0.70316       0.0005542      0.00033002
v  Velocity[z]           -0.41994         0.50502      -0.0012462      -0.0013668
v  TurbEner             0.0010114        0.014886       0.0032852       0.0033449
v  Dissip               9.208e-05        0.030912      0.00045202      0.00039074
v  TurbVisc               0.16383          11.368          4.7111          5.2724
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              641:        0.89737E-01

===============================================================


 INSTANT    0.642000000E+03   TIME STEP NUMBER             642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999749E+04
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 :  0.23756E+00 0.13245E+01
   Friction velocity        uet   :  0.14208E-01 0.78956E-01
   Friction velocity        uk    :  0.17419E-01 0.38737E-01
   Dimensionless distance   yplus :  0.42792E+03 0.95170E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66375E+01      58   0.15181E-02   0.21776E-01 
c  VelocityX    0.46299E+04      12   0.68356E-02   0.38802E-03 
c  VelocityY    0.46299E+04      12   0.68356E-02   0.33659E-04 
c  VelocityZ    0.46299E+04      12   0.68356E-02   0.28711E-04 
c  TurbEner     0.59781E+01      13   0.78919E-04   0.12341E-08 
c  Dissip       0.15083E+01      15   0.77440E-03   0.14505E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.41           54517           26776           27270
v  Velocity[x]            0.29272          2.1874         0.90806         0.90984
v  Velocity[y]           -0.38245         0.69582      0.00055838      0.00033884
v  Velocity[z]           -0.41991         0.51191      -0.0012347      -0.0013558
v  TurbEner             0.0010078        0.014962       0.0032853        0.003345
v  Dissip              9.2055e-05        0.031177      0.00045218      0.00039085
v  TurbVisc               0.16443          11.347          4.7112          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              642:        0.89831E-01

===============================================================


 INSTANT    0.643000000E+03   TIME STEP NUMBER             643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998170E+04
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 :  0.23809E+00 0.12171E+01
   Friction velocity        uet   :  0.14240E-01 0.72554E-01
   Friction velocity        uk    :  0.17388E-01 0.38690E-01
   Dimensionless distance   yplus :  0.42750E+03 0.95174E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55960E+01      57   0.13405E-02   0.18340E-01 
c  VelocityX    0.46298E+04      12   0.68832E-02   0.37989E-03 
c  VelocityY    0.46298E+04      12   0.68832E-02   0.24783E-04 
c  VelocityZ    0.46298E+04      12   0.68832E-02   0.44897E-04 
c  TurbEner     0.59775E+01      13   0.11171E-03   0.13890E-08 
c  Dissip       0.15178E+01      16   0.18308E-02   0.36995E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.29           54526           26776           27270
v  Velocity[x]            0.29286          2.0178         0.90804         0.90982
v  Velocity[y]           -0.36692          0.7024      0.00055697      0.00033561
v  Velocity[z]           -0.42098         0.50579      -0.0012545      -0.0013729
v  TurbEner             0.0010101        0.015481       0.0032854        0.003345
v  Dissip              9.1997e-05        0.032611      0.00045235      0.00039098
v  TurbVisc               0.16411          11.349          4.7113          5.2725
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              643:        0.89820E-01

===============================================================


 INSTANT    0.644000000E+03   TIME STEP NUMBER             644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001345E+04
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 :  0.23770E+00 0.13258E+01
   Friction velocity        uet   :  0.14217E-01 0.79022E-01
   Friction velocity        uk    :  0.17408E-01 0.38696E-01
   Dimensionless distance   yplus :  0.42724E+03 0.95181E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64668E+01      59   0.13343E-02   0.21191E-01 
c  VelocityX    0.46298E+04      12   0.61333E-02   0.36043E-03 
c  VelocityY    0.46298E+04      12   0.61333E-02   0.30583E-04 
c  VelocityZ    0.46298E+04      12   0.61333E-02   0.99606E-04 
c  TurbEner     0.59760E+01      13   0.13523E-03   0.18809E-08 
c  Dissip       0.14824E+01      17   0.22819E-02   0.76827E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.66           54532           26775           27270
v  Velocity[x]            0.29284          2.0936         0.90805         0.90983
v  Velocity[y]            -0.3828         0.69529      0.00055321      0.00033206
v  Velocity[z]             -0.421         0.51056       -0.001237      -0.0013593
v  TurbEner             0.0010099        0.014887       0.0032853       0.0033449
v  Dissip              9.2013e-05        0.031161      0.00045211      0.00039081
v  TurbVisc               0.16407          11.326          4.7113          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              644:        0.90059E-01

===============================================================


 INSTANT    0.645000000E+03   TIME STEP NUMBER             645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000190E+04
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 :  0.23759E+00 0.12143E+01
   Friction velocity        uet   :  0.14211E-01 0.72351E-01
   Friction velocity        uk    :  0.17406E-01 0.38707E-01
   Dimensionless distance   yplus :  0.42761E+03 0.95166E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54890E+01      56   0.11488E-02   0.17998E-01 
c  VelocityX    0.46299E+04      13   0.65628E-02   0.31785E-03 
c  VelocityY    0.46299E+04      13   0.65628E-02   0.26321E-04 
c  VelocityZ    0.46299E+04      13   0.65628E-02   0.45893E-04 
c  TurbEner     0.59760E+01      12   0.67608E-04   0.58956E-09 
c  Dissip       0.14844E+01      14   0.50954E-03   0.39604E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.8           54541           26776           27270
v  Velocity[x]            0.29269          2.1463         0.90806         0.90984
v  Velocity[y]           -0.36737         0.70323      0.00054622      0.00032244
v  Velocity[z]           -0.42135         0.50429      -0.0012469      -0.0013659
v  TurbEner             0.0010074        0.014781        0.003285       0.0033447
v  Dissip              9.2004e-05        0.030882      0.00045204      0.00039076
v  TurbVisc               0.16435          11.316          4.7113          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              645:        0.90049E-01

===============================================================


 INSTANT    0.646000000E+03   TIME STEP NUMBER             646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999496E+04
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 :  0.23800E+00 0.13258E+01
   Friction velocity        uet   :  0.14236E-01 0.79030E-01
   Friction velocity        uk    :  0.17384E-01 0.38729E-01
   Dimensionless distance   yplus :  0.42748E+03 0.95140E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55398E+01      53   0.11359E-02   0.18156E-01 
c  VelocityX    0.46298E+04      12   0.70507E-02   0.31042E-03 
c  VelocityY    0.46298E+04      12   0.70507E-02   0.21458E-04 
c  VelocityZ    0.46298E+04      12   0.70507E-02   0.32181E-04 
c  TurbEner     0.59768E+01      12   0.70414E-04   0.57705E-09 
c  Dissip       0.15056E+01      15   0.70924E-03   0.11413E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.32           54549           26776           27270
v  Velocity[x]            0.29283          2.1845         0.90804         0.90983
v  Velocity[y]           -0.38224         0.69313      0.00054501      0.00032507
v  Velocity[z]           -0.42172         0.51192       -0.001245      -0.0013669
v  TurbEner             0.0010088         0.01486       0.0032851       0.0033447
v  Dissip              9.2026e-05        0.031142      0.00045217      0.00039085
v  TurbVisc               0.16428          11.349          4.7112          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              646:        0.89073E-01

===============================================================


 INSTANT    0.647000000E+03   TIME STEP NUMBER             647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998671E+04
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 :  0.23766E+00 0.12172E+01
   Friction velocity        uet   :  0.14216E-01 0.72558E-01
   Friction velocity        uk    :  0.17396E-01 0.38731E-01
   Dimensionless distance   yplus :  0.42695E+03 0.95151E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63776E+01      58   0.15878E-02   0.20911E-01 
c  VelocityX    0.46298E+04      12   0.69617E-02   0.39516E-03 
c  VelocityY    0.46298E+04      12   0.69617E-02   0.36683E-04 
c  VelocityZ    0.46298E+04      12   0.69617E-02   0.34863E-04 
c  TurbEner     0.59771E+01      13   0.11188E-03   0.11683E-08 
c  Dissip       0.15175E+01      16   0.19367E-02   0.40848E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.18           54540           26776           27270
v  Velocity[x]            0.29305          2.0119         0.90806         0.90983
v  Velocity[y]           -0.36614         0.70074      0.00054367      0.00032157
v  Velocity[z]           -0.41864         0.50648      -0.0012444      -0.0013646
v  TurbEner             0.0010113        0.015405       0.0032852       0.0033448
v  Dissip              9.2031e-05        0.032651      0.00045234      0.00039098
v  TurbVisc               0.16414          11.337          4.7112          5.2725
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              647:        0.89915E-01

===============================================================


 INSTANT    0.648000000E+03   TIME STEP NUMBER             648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000084E+04
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 :  0.23766E+00 0.13240E+01
   Friction velocity        uet   :  0.14217E-01 0.78925E-01
   Friction velocity        uk    :  0.17418E-01 0.38743E-01
   Dimensionless distance   yplus :  0.42802E+03 0.95185E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65307E+01      55   0.15293E-02   0.21418E-01 
c  VelocityX    0.46298E+04      12   0.70251E-02   0.37613E-03 
c  VelocityY    0.46298E+04      12   0.70251E-02   0.40916E-04 
c  VelocityZ    0.46298E+04      12   0.70251E-02   0.63272E-04 
c  TurbEner     0.59762E+01      14   0.13660E-03   0.22564E-08 
c  Dissip       0.14868E+01      16   0.21348E-02   0.67625E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.37           54516           26776           27271
v  Velocity[x]            0.29248          2.0925         0.90805         0.90983
v  Velocity[y]           -0.38231         0.69456      0.00055527      0.00033512
v  Velocity[z]           -0.42102         0.51106      -0.0012348      -0.0013558
v  TurbEner             0.0010081        0.014829       0.0032851       0.0033448
v  Dissip              9.2078e-05        0.031302      0.00045209      0.00039082
v  TurbVisc               0.16483          11.323          4.7113          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              648:        0.89823E-01

===============================================================


 INSTANT    0.649000000E+03   TIME STEP NUMBER             649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998828E+04
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 :  0.23772E+00 0.12166E+01
   Friction velocity        uet   :  0.14220E-01 0.72528E-01
   Friction velocity        uk    :  0.17391E-01 0.38653E-01
   Dimensionless distance   yplus :  0.42765E+03 0.95197E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62692E+01      54   0.12916E-02   0.20560E-01 
c  VelocityX    0.46298E+04      12   0.68052E-02   0.36957E-03 
c  VelocityY    0.46298E+04      12   0.68052E-02   0.34960E-04 
c  VelocityZ    0.46298E+04      12   0.68052E-02   0.42641E-04 
c  TurbEner     0.59754E+01      13   0.64413E-04   0.90802E-09 
c  Dissip       0.14870E+01      14   0.60675E-03   0.48999E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.72           54524           26776           27271
v  Velocity[x]            0.29243          2.1424         0.90806         0.90983
v  Velocity[y]           -0.36774         0.70225      0.00054913      0.00032506
v  Velocity[z]           -0.42165         0.50426      -0.0012502      -0.0013699
v  TurbEner             0.0010116        0.014685        0.003285       0.0033447
v  Dissip              9.2078e-05        0.030916      0.00045201      0.00039075
v  TurbVisc               0.16463           11.36          4.7113          5.2726
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              649:        0.89117E-01

===============================================================


 INSTANT    0.650000000E+03   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999350E+04
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 :  0.23774E+00 0.13247E+01
   Friction velocity        uet   :  0.14221E-01 0.78961E-01
   Friction velocity        uk    :  0.17421E-01 0.38675E-01
   Dimensionless distance   yplus :  0.42756E+03 0.95213E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65617E+01      69   0.13566E-02   0.21485E-01 
c  VelocityX    0.46298E+04      12   0.73315E-02   0.35999E-03 
c  VelocityY    0.46298E+04      12   0.73315E-02   0.25850E-04 
c  VelocityZ    0.46298E+04      12   0.73315E-02   0.29490E-04 
c  TurbEner     0.59761E+01      13   0.65012E-04   0.76102E-09 
c  Dissip       0.15069E+01      15   0.68731E-03   0.11200E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.62           54533           26776           27270
v  Velocity[x]            0.29321          2.1866         0.90804         0.90982
v  Velocity[y]           -0.38247         0.69458      0.00054294      0.00032254
v  Velocity[z]            -0.4206         0.51166      -0.0012379      -0.0013593
v  TurbEner             0.0010128        0.014754        0.003285       0.0033447
v  Dissip              9.2056e-05        0.031107      0.00045211      0.00039082
v  TurbVisc                0.1647          11.342          4.7113          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              650:        0.92563E-01

===============================================================


 INSTANT    0.651000000E+03   TIME STEP NUMBER             651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000692E+04
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 :  0.23792E+00 0.12173E+01
   Friction velocity        uet   :  0.14232E-01 0.72564E-01
   Friction velocity        uk    :  0.17431E-01 0.38720E-01
   Dimensionless distance   yplus :  0.42824E+03 0.95197E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73733E+01      60   0.15916E-02   0.24181E-01 
c  VelocityX    0.46298E+04      12   0.70486E-02   0.38753E-03 
c  VelocityY    0.46298E+04      12   0.70486E-02   0.40412E-04 
c  VelocityZ    0.46298E+04      12   0.70486E-02   0.10224E-03 
c  TurbEner     0.59767E+01      13   0.11385E-03   0.12074E-08 
c  Dissip       0.15191E+01      15   0.16696E-02   0.30276E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.76           54539           26776           27270
v  Velocity[x]            0.29277          2.0278         0.90806         0.90983
v  Velocity[y]           -0.36665         0.70086      0.00055462      0.00033116
v  Velocity[z]           -0.42139         0.50589      -0.0012501      -0.0013718
v  TurbEner             0.0010108        0.015276       0.0032851       0.0033448
v  Dissip              9.2052e-05        0.032403      0.00045228      0.00039094
v  TurbVisc               0.16511          11.339          4.7113          5.2726
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              651:        0.90793E-01

===============================================================


 INSTANT    0.652000000E+03   TIME STEP NUMBER             652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000427E+04
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 :  0.23776E+00 0.13251E+01
   Friction velocity        uet   :  0.14223E-01 0.78982E-01
   Friction velocity        uk    :  0.17414E-01 0.38767E-01
   Dimensionless distance   yplus :  0.42820E+03 0.95246E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64474E+01      54   0.13800E-02   0.21127E-01 
c  VelocityX    0.46297E+04      12   0.70501E-02   0.35849E-03 
c  VelocityY    0.46297E+04      12   0.70501E-02   0.48496E-04 
c  VelocityZ    0.46297E+04      12   0.70501E-02   0.58170E-04 
c  TurbEner     0.59759E+01      13   0.12464E-03   0.16562E-08 
c  Dissip       0.14822E+01      16   0.21679E-02   0.69830E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.38           54548           26776           27270
v  Velocity[x]             0.2925          2.0954         0.90806         0.90984
v  Velocity[y]           -0.38226         0.69434      0.00054509      0.00032495
v  Velocity[z]           -0.42075         0.51108      -0.0012435      -0.0013657
v  TurbEner              0.001012        0.014761       0.0032852       0.0033449
v  Dissip              9.2074e-05        0.031045       0.0004521      0.00039082
v  TurbVisc                 0.165          11.366          4.7114          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              652:        0.89251E-01

===============================================================


 INSTANT    0.653000000E+03   TIME STEP NUMBER             653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999349E+04
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 :  0.23781E+00 0.12491E+01
   Friction velocity        uet   :  0.14225E-01 0.72808E-01
   Friction velocity        uk    :  0.17424E-01 0.38773E-01
   Dimensionless distance   yplus :  0.42761E+03 0.95257E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60743E+01      55   0.15662E-02   0.19904E-01 
c  VelocityX    0.46298E+04      12   0.71109E-02   0.38349E-03 
c  VelocityY    0.46298E+04      12   0.71109E-02   0.32246E-04 
c  VelocityZ    0.46298E+04      12   0.71109E-02   0.43616E-04 
c  TurbEner     0.59765E+01      12   0.80332E-04   0.74816E-09 
c  Dissip       0.14823E+01      14   0.56367E-03   0.40476E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.82           54539           26775           27269
v  Velocity[x]            0.29308          2.1563         0.90808         0.90985
v  Velocity[y]           -0.36695         0.70207      0.00055693      0.00033438
v  Velocity[z]           -0.41917         0.50471      -0.0012437      -0.0013612
v  TurbEner             0.0010132        0.014645       0.0032853        0.003345
v  Dissip              9.2076e-05        0.030681      0.00045205       0.0003908
v  TurbVisc                0.1647          11.344          4.7115          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              653:        0.89560E-01

===============================================================


 INSTANT    0.654000000E+03   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002029E+04
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 :  0.23740E+00 0.13253E+01
   Friction velocity        uet   :  0.14201E-01 0.78999E-01
   Friction velocity        uk    :  0.17434E-01 0.38763E-01
   Dimensionless distance   yplus :  0.42842E+03 0.95260E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61653E+01      57   0.14575E-02   0.20206E-01 
c  VelocityX    0.46299E+04      12   0.72054E-02   0.38811E-03 
c  VelocityY    0.46299E+04      12   0.72054E-02   0.27991E-04 
c  VelocityZ    0.46299E+04      12   0.72054E-02   0.37445E-04 
c  TurbEner     0.59780E+01      13   0.85257E-04   0.12208E-08 
c  Dissip       0.15057E+01      15   0.86671E-03   0.16458E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.1           54515           26776           27270
v  Velocity[x]            0.29281          2.1896         0.90807         0.90985
v  Velocity[y]           -0.38247         0.69165       0.0005501      0.00033129
v  Velocity[z]           -0.42176         0.51176      -0.0012415      -0.0013598
v  TurbEner             0.0010086        0.014785       0.0032856       0.0033452
v  Dissip              9.2069e-05        0.031061      0.00045222      0.00039092
v  TurbVisc               0.16513          11.355          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              654:        0.89779E-01

===============================================================


 INSTANT    0.655000000E+03   TIME STEP NUMBER             655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998602E+04
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 :  0.23761E+00 0.12170E+01
   Friction velocity        uet   :  0.14213E-01 0.72543E-01
   Friction velocity        uk    :  0.17395E-01 0.38683E-01
   Dimensionless distance   yplus :  0.42782E+03 0.95271E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61229E+01      55   0.13138E-02   0.20080E-01 
c  VelocityX    0.46298E+04      12   0.68667E-02   0.41651E-03 
c  VelocityY    0.46298E+04      12   0.68667E-02   0.32721E-04 
c  VelocityZ    0.46298E+04      12   0.68667E-02   0.31745E-04 
c  TurbEner     0.59779E+01      13   0.12143E-03   0.16428E-08 
c  Dissip       0.15200E+01      16   0.21097E-02   0.49468E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.03           54522           26776           27270
v  Velocity[x]            0.29263          2.0181         0.90806         0.90984
v  Velocity[y]           -0.36693         0.69932      0.00055506      0.00033344
v  Velocity[z]           -0.42139         0.50571      -0.0012567      -0.0013753
v  TurbEner             0.0010106        0.015362       0.0032858       0.0033454
v  Dissip              9.2103e-05        0.032697      0.00045239      0.00039104
v  TurbVisc               0.16467          11.335          4.7116          5.2729
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              655:        0.89501E-01

===============================================================


 INSTANT    0.656000000E+03   TIME STEP NUMBER             656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000576E+04
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 :  0.23805E+00 0.13236E+01
   Friction velocity        uet   :  0.14238E-01 0.78897E-01
   Friction velocity        uk    :  0.17412E-01 0.38588E-01
   Dimensionless distance   yplus :  0.42750E+03 0.95195E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63857E+01      59   0.13319E-02   0.20926E-01 
c  VelocityX    0.46298E+04      12   0.71411E-02   0.31674E-03 
c  VelocityY    0.46298E+04      12   0.71411E-02   0.34519E-04 
c  VelocityZ    0.46298E+04      12   0.71411E-02   0.58042E-04 
c  TurbEner     0.59769E+01      14   0.13442E-03   0.20228E-08 
c  Dissip       0.14944E+01      16   0.19201E-02   0.54954E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.51           54532           26776           27270
v  Velocity[x]            0.29293          2.0946         0.90804         0.90982
v  Velocity[y]           -0.38288         0.69443      0.00055103      0.00033295
v  Velocity[z]           -0.42053         0.51041      -0.0012441      -0.0013675
v  TurbEner             0.0010106        0.014824       0.0032856       0.0033452
v  Dissip              9.2097e-05        0.031487      0.00045216      0.00039088
v  TurbVisc                0.1646          11.338          4.7117          5.2729
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              656:        0.89886E-01

===============================================================


 INSTANT    0.657000000E+03   TIME STEP NUMBER             657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999765E+04
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 :  0.23792E+00 0.12125E+01
   Friction velocity        uet   :  0.14231E-01 0.72280E-01
   Friction velocity        uk    :  0.17412E-01 0.38698E-01
   Dimensionless distance   yplus :  0.42795E+03 0.95198E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62716E+01      56   0.13448E-02   0.20570E-01 
c  VelocityX    0.46298E+04      13   0.66592E-02   0.29835E-03 
c  VelocityY    0.46298E+04      13   0.66592E-02   0.26454E-04 
c  VelocityZ    0.46298E+04      13   0.66592E-02   0.87104E-04 
c  TurbEner     0.59768E+01      12   0.68489E-04   0.64125E-09 
c  Dissip       0.14973E+01      13   0.63582E-03   0.44179E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -180.06           54539           26775           27269
v  Velocity[x]            0.29257          2.1497         0.90806         0.90984
v  Velocity[y]           -0.36737         0.70418      0.00055912      0.00033618
v  Velocity[z]           -0.42305         0.50437      -0.0012488      -0.0013693
v  TurbEner             0.0010074        0.014665       0.0032855       0.0033452
v  Dissip               9.208e-05         0.03105      0.00045208      0.00039082
v  TurbVisc               0.16487          11.317          4.7116          5.2729
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              657:        0.89911E-01

===============================================================


 INSTANT    0.658000000E+03   TIME STEP NUMBER             658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001028E+04
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 :  0.23765E+00 0.13246E+01
   Friction velocity        uet   :  0.14214E-01 0.78956E-01
   Friction velocity        uk    :  0.17384E-01 0.38760E-01
   Dimensionless distance   yplus :  0.42770E+03 0.95193E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62786E+01      54   0.13651E-02   0.20577E-01 
c  VelocityX    0.46298E+04      12   0.73257E-02   0.34600E-03 
c  VelocityY    0.46298E+04      12   0.73257E-02   0.37360E-04 
c  VelocityZ    0.46298E+04      12   0.73257E-02   0.45824E-04 
c  TurbEner     0.59775E+01      12   0.64830E-04   0.66883E-09 
c  Dissip       0.15137E+01      15   0.73017E-03   0.11952E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.11           54549           26776           27270
v  Velocity[x]            0.29251          2.1806         0.90806         0.90984
v  Velocity[y]           -0.38228         0.69168      0.00055228         0.00033
v  Velocity[z]           -0.41962         0.51186      -0.0012485      -0.0013707
v  TurbEner             0.0010081        0.014801       0.0032856       0.0033453
v  Dissip               9.207e-05         0.03134      0.00045221      0.00039091
v  TurbVisc               0.16456          11.314          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              658:        0.89229E-01

===============================================================


 INSTANT    0.659000000E+03   TIME STEP NUMBER             659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998902E+04
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 :  0.23774E+00 0.12183E+01
   Friction velocity        uet   :  0.14219E-01 0.72613E-01
   Friction velocity        uk    :  0.17390E-01 0.38770E-01
   Dimensionless distance   yplus :  0.42697E+03 0.95155E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63940E+01      51   0.15137E-02   0.20951E-01 
c  VelocityX    0.46299E+04      12   0.75252E-02   0.38676E-03 
c  VelocityY    0.46299E+04      12   0.75252E-02   0.40226E-04 
c  VelocityZ    0.46299E+04      12   0.75252E-02   0.42692E-04 
c  TurbEner     0.59791E+01      12   0.74379E-04   0.75955E-09 
c  Dissip       0.15420E+01      15   0.92940E-03   0.16497E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.91           54539           26775           27269
v  Velocity[x]            0.29331          2.2125         0.90807         0.90984
v  Velocity[y]           -0.36614         0.70085      0.00056369      0.00033943
v  Velocity[z]           -0.42028         0.50641      -0.0012511      -0.0013709
v  TurbEner             0.0010095        0.014983       0.0032858       0.0033455
v  Dissip              9.2103e-05        0.031871      0.00045245      0.00039107
v  TurbVisc               0.16432          11.323          4.7115          5.2728
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              659:        0.88847E-01

===============================================================


 INSTANT    0.660000000E+03   TIME STEP NUMBER             660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000554E+04
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 :  0.23755E+00 0.13240E+01
   Friction velocity        uet   :  0.14208E-01 0.78915E-01
   Friction velocity        uk    :  0.17403E-01 0.38745E-01
   Dimensionless distance   yplus :  0.42778E+03 0.95239E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60564E+01      58   0.15599E-02   0.19864E-01 
c  VelocityX    0.46298E+04      12   0.69607E-02   0.40628E-03 
c  VelocityY    0.46298E+04      12   0.69607E-02   0.24135E-04 
c  VelocityZ    0.46298E+04      12   0.69607E-02   0.51316E-04 
c  TurbEner     0.59801E+01      13   0.14461E-03   0.17790E-08 
c  Dissip       0.15637E+01      16   0.24778E-02   0.66543E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.53           54516           26776           27270
v  Velocity[x]            0.29277           2.036         0.90805         0.90983
v  Velocity[y]           -0.38233         0.69465      0.00056149       0.0003389
v  Velocity[z]           -0.42181         0.51099      -0.0012453      -0.0013636
v  TurbEner             0.0010049        0.015684       0.0032861       0.0033457
v  Dissip              9.2135e-05        0.033855      0.00045278      0.00039134
v  TurbVisc               0.16478          11.368          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              660:        0.90078E-01

===============================================================


 INSTANT    0.661000000E+03   TIME STEP NUMBER             661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998582E+04
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 :  0.23777E+00 0.12172E+01
   Friction velocity        uet   :  0.14221E-01 0.72564E-01
   Friction velocity        uk    :  0.17363E-01 0.38665E-01
   Dimensionless distance   yplus :  0.42713E+03 0.95290E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64512E+01      56   0.12081E-02   0.21146E-01 
c  VelocityX    0.46297E+04      12   0.68054E-02   0.41950E-03 
c  VelocityY    0.46297E+04      12   0.68054E-02   0.36855E-04 
c  VelocityZ    0.46297E+04      12   0.68054E-02   0.42845E-04 
c  TurbEner     0.59782E+01      14   0.15288E-03   0.23358E-08 
c  Dissip       0.15290E+01      16   0.22025E-02   0.67003E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.99           54523           26776           27270
v  Velocity[x]            0.29253          2.1033         0.90804         0.90982
v  Velocity[y]           -0.36773         0.70312      0.00055435      0.00033182
v  Velocity[z]           -0.42098          0.5041      -0.0012606      -0.0013796
v  TurbEner             0.0010067         0.01501       0.0032862       0.0033458
v  Dissip              9.2095e-05        0.032362       0.0004526      0.00039121
v  TurbVisc               0.16425          11.355          4.7116          5.2728
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              661:        0.89926E-01

===============================================================


 INSTANT    0.662000000E+03   TIME STEP NUMBER             662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002009E+04
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 :  0.23790E+00 0.13240E+01
   Friction velocity        uet   :  0.14229E-01 0.78915E-01
   Friction velocity        uk    :  0.17378E-01 0.38722E-01
   Dimensionless distance   yplus :  0.42672E+03 0.95232E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66096E+01      60   0.13628E-02   0.21652E-01 
c  VelocityX    0.46299E+04      12   0.68174E-02   0.37731E-03 
c  VelocityY    0.46299E+04      12   0.68174E-02   0.37859E-04 
c  VelocityZ    0.46299E+04      12   0.68174E-02   0.31190E-04 
c  TurbEner     0.59786E+01      13   0.69390E-04   0.75551E-09 
c  Dissip       0.15420E+01      13   0.30745E-03   0.20691E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.13           54531           26775           27269
v  Velocity[x]            0.29287          2.1607         0.90806         0.90984
v  Velocity[y]           -0.38252         0.69563      0.00055158      0.00033042
v  Velocity[z]           -0.42133         0.51163      -0.0012494      -0.0013688
v  TurbEner             0.0010063        0.014894       0.0032861       0.0033458
v  Dissip              9.2037e-05        0.032231      0.00045262      0.00039122
v  TurbVisc               0.16416          11.362          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              662:        0.90007E-01

===============================================================


 INSTANT    0.663000000E+03   TIME STEP NUMBER             663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000656E+04
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 :  0.23767E+00 0.12188E+01
   Friction velocity        uet   :  0.14215E-01 0.72555E-01
   Friction velocity        uk    :  0.17375E-01 0.38782E-01
   Dimensionless distance   yplus :  0.42698E+03 0.95201E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57240E+01      54   0.12759E-02   0.18764E-01 
c  VelocityX    0.46298E+04      12   0.66817E-02   0.31872E-03 
c  VelocityY    0.46298E+04      12   0.66817E-02   0.28645E-04 
c  VelocityZ    0.46298E+04      12   0.66817E-02   0.31419E-04 
c  TurbEner     0.59793E+01      12   0.82723E-04   0.91400E-09 
c  Dissip       0.15633E+01      15   0.83716E-03   0.16943E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.35           54539           26775           27269
v  Velocity[x]            0.29259          2.1885         0.90806         0.90983
v  Velocity[y]           -0.36655         0.70136      0.00054738      0.00032463
v  Velocity[z]           -0.42253         0.50594      -0.0012592       -0.001376
v  TurbEner             0.0010036        0.014978       0.0032862       0.0033458
v  Dissip              9.2039e-05        0.032505      0.00045279      0.00039134
v  TurbVisc               0.16432          11.336          4.7115          5.2727
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              663:        0.89382E-01

===============================================================


 INSTANT    0.664000000E+03   TIME STEP NUMBER             664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000866E+04
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 :  0.23776E+00 0.13253E+01
   Friction velocity        uet   :  0.14220E-01 0.78993E-01
   Friction velocity        uk    :  0.17352E-01 0.38790E-01
   Dimensionless distance   yplus :  0.42678E+03 0.95113E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59379E+01      55   0.13234E-02   0.19475E-01 
c  VelocityX    0.46297E+04      12   0.67161E-02   0.32644E-03 
c  VelocityY    0.46297E+04      12   0.67161E-02   0.29569E-04 
c  VelocityZ    0.46297E+04      12   0.67161E-02   0.56115E-04 
c  TurbEner     0.59796E+01      13   0.11920E-03   0.10829E-08 
c  Dissip       0.15711E+01      16   0.19677E-02   0.40637E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.45           54549           26776           27270
v  Velocity[x]            0.29261          2.0218         0.90806         0.90983
v  Velocity[y]           -0.38218         0.69266      0.00054769      0.00032683
v  Velocity[z]            -0.4203         0.51101      -0.0012608      -0.0013817
v  TurbEner             0.0010047        0.015545       0.0032864        0.003346
v  Dissip               9.207e-05        0.034057      0.00045302      0.00039151
v  TurbVisc               0.16409          11.333          4.7115          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              664:        0.89904E-01

===============================================================


 INSTANT    0.665000000E+03   TIME STEP NUMBER             665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998476E+04
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 :  0.23754E+00 0.12303E+01
   Friction velocity        uet   :  0.14207E-01 0.72492E-01
   Friction velocity        uk    :  0.17361E-01 0.38664E-01
   Dimensionless distance   yplus :  0.42615E+03 0.95055E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57933E+01      54   0.14318E-02   0.18977E-01 
c  VelocityX    0.46297E+04      12   0.72825E-02   0.36652E-03 
c  VelocityY    0.46297E+04      12   0.72825E-02   0.27389E-04 
c  VelocityZ    0.46297E+04      12   0.72825E-02   0.49356E-04 
c  TurbEner     0.59784E+01      13   0.15491E-03   0.20885E-08 
c  Dissip       0.15333E+01      16   0.25549E-02   0.83788E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.21           54539           26775           27269
v  Velocity[x]            0.29297          2.1023         0.90807         0.90985
v  Velocity[y]           -0.36694         0.70133      0.00054719      0.00032452
v  Velocity[z]           -0.41977         0.50475      -0.0012549      -0.0013733
v  TurbEner             0.0010067        0.014857       0.0032863        0.003346
v  Dissip              9.2037e-05        0.032299      0.00045282      0.00039138
v  TurbVisc               0.16385          11.362          4.7114          5.2726
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              665:        0.89560E-01

===============================================================


 INSTANT    0.666000000E+03   TIME STEP NUMBER             666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001692E+04
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 :  0.23769E+00 0.13233E+01
   Friction velocity        uet   :  0.14216E-01 0.78878E-01
   Friction velocity        uk    :  0.17379E-01 0.38684E-01
   Dimensionless distance   yplus :  0.42711E+03 0.95026E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66194E+01      57   0.16290E-02   0.21715E-01 
c  VelocityX    0.46298E+04      12   0.70392E-02   0.39506E-03 
c  VelocityY    0.46298E+04      12   0.70392E-02   0.30601E-04 
c  VelocityZ    0.46298E+04      12   0.70392E-02   0.91895E-04 
c  TurbEner     0.59787E+01      13   0.64086E-04   0.88518E-09 
c  Dissip       0.15344E+01      14   0.57474E-03   0.41672E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.41           54519           26776           27270
v  Velocity[x]            0.29245          2.1618         0.90805         0.90983
v  Velocity[y]           -0.38246         0.69405      0.00055368      0.00033495
v  Velocity[z]           -0.42043         0.51169      -0.0012385      -0.0013584
v  TurbEner             0.0010027        0.014734       0.0032863        0.003346
v  Dissip               9.205e-05          0.0319      0.00045278      0.00039136
v  TurbVisc               0.16437          11.346          4.7113          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              666:        0.89907E-01

===============================================================


 INSTANT    0.667000000E+03   TIME STEP NUMBER             667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999388E+04
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 :  0.23798E+00 0.12495E+01
   Friction velocity        uet   :  0.14233E-01 0.72721E-01
   Friction velocity        uk    :  0.17344E-01 0.38648E-01
   Dimensionless distance   yplus :  0.42660E+03 0.95052E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59435E+01      58   0.14700E-02   0.19483E-01 
c  VelocityX    0.46297E+04      12   0.71605E-02   0.42904E-03 
c  VelocityY    0.46297E+04      12   0.71605E-02   0.27014E-04 
c  VelocityZ    0.46297E+04      12   0.71605E-02   0.40378E-04 
c  TurbEner     0.59781E+01      13   0.10576E-03   0.15498E-08 
c  Dissip       0.15390E+01      16   0.16142E-02   0.31481E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.83           54520           26775           27269
v  Velocity[x]             0.2927           2.011         0.90806         0.90984
v  Velocity[y]           -0.36695         0.70028      0.00055209      0.00033007
v  Velocity[z]           -0.42147         0.50566       -0.001252      -0.0013718
v  TurbEner             0.0010052        0.015191       0.0032862       0.0033459
v  Dissip              9.2034e-05        0.033089      0.00045286      0.00039142
v  TurbVisc               0.16388          11.354          4.7112          5.2724
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              667:        0.89986E-01

===============================================================


 INSTANT    0.668000000E+03   TIME STEP NUMBER             668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001749E+04
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 :  0.23782E+00 0.13254E+01
   Friction velocity        uet   :  0.14224E-01 0.79011E-01
   Friction velocity        uk    :  0.17366E-01 0.38694E-01
   Dimensionless distance   yplus :  0.42632E+03 0.95103E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57547E+01      54   0.12629E-02   0.18860E-01 
c  VelocityX    0.46297E+04      12   0.70603E-02   0.37036E-03 
c  VelocityY    0.46297E+04      12   0.70603E-02   0.26915E-04 
c  VelocityZ    0.46297E+04      12   0.70603E-02   0.51916E-04 
c  TurbEner     0.59766E+01      14   0.14398E-03   0.21224E-08 
c  Dissip       0.14969E+01      17   0.24776E-02   0.84965E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.3           54521           26775           27269
v  Velocity[x]            0.29271          2.0879         0.90804         0.90982
v  Velocity[y]           -0.38282         0.69372      0.00055851      0.00033834
v  Velocity[z]           -0.42142         0.51049      -0.0012419      -0.0013616
v  TurbEner             0.0010056        0.014585        0.003286       0.0033458
v  Dissip               9.205e-05        0.031509      0.00045248      0.00039116
v  TurbVisc               0.16383          11.392          4.7111          5.2722
v  total_pressure           83075      1.5657e+05      1.1921e+05      1.1998e+05


 TIME FOR THE TIME STEP              668:        0.88614E-01

===============================================================


 INSTANT    0.669000000E+03   TIME STEP NUMBER             669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001682E+04
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 :  0.23761E+00 0.12148E+01
   Friction velocity        uet   :  0.14211E-01 0.72312E-01
   Friction velocity        uk    :  0.17369E-01 0.38715E-01
   Dimensionless distance   yplus :  0.42682E+03 0.95133E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59981E+01      68   0.13596E-02   0.19679E-01 
c  VelocityX    0.46297E+04      13   0.70372E-02   0.36236E-03 
c  VelocityY    0.46297E+04      13   0.70372E-02   0.27383E-04 
c  VelocityZ    0.46297E+04      13   0.70372E-02   0.46231E-04 
c  TurbEner     0.59767E+01      12   0.76445E-04   0.76085E-09 
c  Dissip       0.14955E+01      14   0.76684E-03   0.69178E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.92           54508           26775           27269
v  Velocity[x]            0.29276          2.1386         0.90805         0.90983
v  Velocity[y]           -0.36737         0.70243       0.0005658      0.00034216
v  Velocity[z]           -0.42168         0.50429      -0.0012509       -0.001366
v  TurbEner             0.0010027        0.014451       0.0032857       0.0033456
v  Dissip              9.2016e-05        0.031003      0.00045228      0.00039101
v  TurbVisc               0.16408          11.371          4.7111          5.2722
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              669:        0.92469E-01

===============================================================


 INSTANT    0.670000000E+03   TIME STEP NUMBER             670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998528E+04
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 :  0.23779E+00 0.13248E+01
   Friction velocity        uet   :  0.14222E-01 0.78973E-01
   Friction velocity        uk    :  0.17344E-01 0.38727E-01
   Dimensionless distance   yplus :  0.42660E+03 0.95193E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58496E+01      69   0.11549E-02   0.19165E-01 
c  VelocityX    0.46297E+04      12   0.71242E-02   0.34955E-03 
c  VelocityY    0.46297E+04      12   0.71242E-02   0.40126E-04 
c  VelocityZ    0.46297E+04      12   0.71242E-02   0.81814E-04 
c  TurbEner     0.59767E+01      13   0.80524E-04   0.12350E-08 
c  Dissip       0.15103E+01      15   0.67737E-03   0.11491E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.97           54517           26776           27270
v  Velocity[x]            0.29283          2.1807         0.90802          0.9098
v  Velocity[y]           -0.38229         0.69199      0.00055893      0.00033754
v  Velocity[z]           -0.41966         0.51187      -0.0012375      -0.0013606
v  TurbEner             0.0010035        0.014554       0.0032855       0.0033455
v  Dissip              9.2031e-05        0.031117      0.00045225      0.00039097
v  TurbVisc               0.16371          11.372           4.711          5.2721
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              670:        0.92310E-01

===============================================================


 INSTANT    0.671000000E+03   TIME STEP NUMBER             671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999562E+04
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 :  0.23749E+00 0.12197E+01
   Friction velocity        uet   :  0.14203E-01 0.72526E-01
   Friction velocity        uk    :  0.17351E-01 0.38614E-01
   Dimensionless distance   yplus :  0.42592E+03 0.95223E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57159E+01      56   0.13480E-02   0.18740E-01 
c  VelocityX    0.46296E+04      12   0.68787E-02   0.36173E-03 
c  VelocityY    0.46296E+04      12   0.68787E-02   0.23875E-04 
c  VelocityZ    0.46296E+04      12   0.68787E-02   0.40118E-04 
c  TurbEner     0.59773E+01      13   0.12568E-03   0.12523E-08 
c  Dissip       0.15208E+01      16   0.19341E-02   0.38742E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.04           54529           26775           27269
v  Velocity[x]            0.29282          2.0161         0.90804         0.90981
v  Velocity[y]           -0.36607          0.7006       0.0005502      0.00032755
v  Velocity[z]           -0.41963         0.50649      -0.0012529      -0.0013717
v  TurbEner             0.0010052        0.015129       0.0032855       0.0033455
v  Dissip              9.2067e-05        0.032599      0.00045232      0.00039103
v  TurbVisc               0.16348          11.345          4.7109          5.2721
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              671:        0.89699E-01

===============================================================


 INSTANT    0.672000000E+03   TIME STEP NUMBER             672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000636E+04
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 :  0.23793E+00 0.13238E+01
   Friction velocity        uet   :  0.14229E-01 0.78912E-01
   Friction velocity        uk    :  0.17365E-01 0.38691E-01
   Dimensionless distance   yplus :  0.42684E+03 0.95248E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55905E+01      54   0.12168E-02   0.18330E-01 
c  VelocityX    0.46297E+04      13   0.63108E-02   0.33453E-03 
c  VelocityY    0.46297E+04      13   0.63108E-02   0.22448E-04 
c  VelocityZ    0.46297E+04      13   0.63108E-02   0.50838E-04 
c  TurbEner     0.59760E+01      13   0.13424E-03   0.17761E-08 
c  Dissip       0.14828E+01      17   0.23547E-02   0.78426E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.11           54540           26776           27270
v  Velocity[x]            0.29257          2.0926         0.90804         0.90982
v  Velocity[y]           -0.38228          0.6953       0.0005507      0.00032922
v  Velocity[z]           -0.42093         0.51098      -0.0012527      -0.0013749
v  TurbEner             0.0010003        0.014557       0.0032852       0.0033452
v  Dissip              9.2086e-05        0.031131      0.00045196      0.00039078
v  TurbVisc               0.16395          11.338          4.7109          5.2721
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              672:        0.89978E-01

===============================================================


 INSTANT    0.673000000E+03   TIME STEP NUMBER             673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998994E+04
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 :  0.23794E+00 0.12133E+01
   Friction velocity        uet   :  0.14230E-01 0.72330E-01
   Friction velocity        uk    :  0.17323E-01 0.38687E-01
   Dimensionless distance   yplus :  0.42619E+03 0.95269E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.52979E+01      54   0.11688E-02   0.17360E-01 
c  VelocityX    0.46297E+04      13   0.73216E-02   0.27439E-03 
c  VelocityY    0.46297E+04      13   0.73216E-02   0.24858E-04 
c  VelocityZ    0.46297E+04      13   0.73216E-02   0.45397E-04 
c  TurbEner     0.59760E+01      12   0.64120E-04   0.56456E-09 
c  Dissip       0.14825E+01      14   0.66347E-03   0.49702E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.41           54547           26775           27269
v  Velocity[x]            0.29285           2.142         0.90805         0.90983
v  Velocity[y]           -0.36769         0.70392      0.00055467       0.0003319
v  Velocity[z]           -0.42237          0.5042      -0.0012583      -0.0013757
v  TurbEner             0.0010011        0.014457        0.003285       0.0033451
v  Dissip              9.2116e-05        0.030692      0.00045182      0.00039068
v  TurbVisc               0.16328          11.368          4.7109          5.2721
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              673:        0.89983E-01

===============================================================


 INSTANT    0.674000000E+03   TIME STEP NUMBER             674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001098E+04
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 :  0.23760E+00 0.13253E+01
   Friction velocity        uet   :  0.14210E-01 0.78997E-01
   Friction velocity        uk    :  0.17330E-01 0.38723E-01
   Dimensionless distance   yplus :  0.42555E+03 0.95309E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65263E+01      55   0.15358E-02   0.21381E-01 
c  VelocityX    0.46297E+04      12   0.74717E-02   0.38229E-03 
c  VelocityY    0.46297E+04      12   0.74717E-02   0.44331E-04 
c  VelocityZ    0.46297E+04      12   0.74717E-02   0.80921E-04 
c  TurbEner     0.59772E+01      13   0.72740E-04   0.87792E-09 
c  Dissip       0.15001E+01      15   0.72250E-03   0.12140E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.49           54539           26775           27269
v  Velocity[x]            0.29298          2.1823         0.90805         0.90983
v  Velocity[y]           -0.38244         0.69188      0.00055812      0.00033884
v  Velocity[z]           -0.41912         0.51163      -0.0012445      -0.0013649
v  TurbEner             0.0010009        0.014609       0.0032852       0.0033452
v  Dissip              9.2136e-05        0.030895      0.00045191      0.00039074
v  TurbVisc               0.16315          11.342          4.7108           5.272
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              674:        0.89283E-01

===============================================================


 INSTANT    0.675000000E+03   TIME STEP NUMBER             675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999028E+04
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 :  0.23770E+00 0.12283E+01
   Friction velocity        uet   :  0.14216E-01 0.72573E-01
   Friction velocity        uk    :  0.17328E-01 0.38767E-01
   Dimensionless distance   yplus :  0.42597E+03 0.95265E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59727E+01      68   0.15604E-02   0.19596E-01 
c  VelocityX    0.46298E+04      12   0.68952E-02   0.42171E-03 
c  VelocityY    0.46298E+04      12   0.68952E-02   0.27714E-04 
c  VelocityZ    0.46298E+04      12   0.68952E-02   0.40233E-04 
c  TurbEner     0.59779E+01      13   0.13079E-03   0.17923E-08 
c  Dissip       0.15135E+01      16   0.20199E-02   0.43485E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.96           54516           26776           27270
v  Velocity[x]            0.29257          2.0154         0.90807         0.90985
v  Velocity[y]           -0.36664         0.70092      0.00055778       0.0003362
v  Velocity[z]           -0.42108         0.50593      -0.0012504      -0.0013679
v  TurbEner            0.00099704        0.015228       0.0032852       0.0033452
v  Dissip              9.2139e-05        0.032446      0.00045207      0.00039087
v  TurbVisc               0.16339          11.339          4.7109          5.2721
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              675:        0.92706E-01

===============================================================


 INSTANT    0.676000000E+03   TIME STEP NUMBER             676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999743E+04
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 :  0.23768E+00 0.13236E+01
   Friction velocity        uet   :  0.14215E-01 0.78891E-01
   Friction velocity        uk    :  0.17295E-01 0.38762E-01
   Dimensionless distance   yplus :  0.42551E+03 0.95291E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58424E+01      53   0.12510E-02   0.19159E-01 
c  VelocityX    0.46297E+04      12   0.65774E-02   0.37033E-03 
c  VelocityY    0.46297E+04      12   0.65774E-02   0.24415E-04 
c  VelocityZ    0.46297E+04      12   0.65774E-02   0.50993E-04 
c  TurbEner     0.59761E+01      13   0.13031E-03   0.19048E-08 
c  Dissip       0.14754E+01      17   0.23230E-02   0.76873E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.58           54526           26776           27270
v  Velocity[x]            0.29266          2.0918         0.90802          0.9098
v  Velocity[y]           -0.38231         0.69525      0.00055664      0.00033589
v  Velocity[z]           -0.42088         0.51106      -0.0012533      -0.0013749
v  TurbEner            0.00099733        0.014661       0.0032852       0.0033452
v  Dissip              9.2118e-05        0.030982      0.00045182       0.0003907
v  TurbVisc               0.16295          11.361          4.7108           5.272
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              676:        0.89178E-01

===============================================================


 INSTANT    0.677000000E+03   TIME STEP NUMBER             677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000188E+04
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 :  0.23809E+00 0.12174E+01
   Friction velocity        uet   :  0.14240E-01 0.72572E-01
   Friction velocity        uk    :  0.17297E-01 0.38798E-01
   Dimensionless distance   yplus :  0.42475E+03 0.95329E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60879E+01      52   0.12011E-02   0.19951E-01 
c  VelocityX    0.46298E+04      12   0.66819E-02   0.35579E-03 
c  VelocityY    0.46298E+04      12   0.66819E-02   0.24174E-04 
c  VelocityZ    0.46298E+04      12   0.66819E-02   0.50880E-04 
c  TurbEner     0.59760E+01      13   0.61976E-04   0.70507E-09 
c  Dissip       0.14738E+01      14   0.62309E-03   0.45007E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.99           54535           26776           27270
v  Velocity[x]            0.29302          2.1396         0.90806         0.90984
v  Velocity[y]           -0.36693         0.70319      0.00055164      0.00032976
v  Velocity[z]           -0.42061         0.50473      -0.0012561      -0.0013722
v  TurbEner            0.00099927        0.014565       0.0032851       0.0033451
v  Dissip              9.2126e-05        0.030571      0.00045173      0.00039063
v  TurbVisc               0.16277          11.348          4.7109          5.2721
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              677:        0.89292E-01

===============================================================


 INSTANT    0.678000000E+03   TIME STEP NUMBER             678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000186E+04
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 :  0.23797E+00 0.13241E+01
   Friction velocity        uet   :  0.14233E-01 0.78921E-01
   Friction velocity        uk    :  0.17314E-01 0.38838E-01
   Dimensionless distance   yplus :  0.42564E+03 0.95302E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65728E+01      57   0.14131E-02   0.21546E-01 
c  VelocityX    0.46298E+04      12   0.71915E-02   0.30866E-03 
c  VelocityY    0.46298E+04      12   0.71915E-02   0.77281E-04 
c  VelocityZ    0.46298E+04      12   0.71915E-02   0.10783E-03 
c  TurbEner     0.59773E+01      13   0.77133E-04   0.79869E-09 
c  Dissip       0.14913E+01      14   0.62725E-03   0.92509E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.4           54539           26775           27270
v  Velocity[x]            0.29253          2.1827         0.90804         0.90982
v  Velocity[y]           -0.38242         0.69549      0.00055135      0.00032998
v  Velocity[z]           -0.42278         0.51176      -0.0012464      -0.0013686
v  TurbEner            0.00099554        0.014696       0.0032852       0.0033452
v  Dissip              9.2097e-05        0.030726      0.00045184       0.0003907
v  TurbVisc               0.16332          11.351          4.7109          5.2721
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              678:        0.89758E-01

===============================================================


 INSTANT    0.679000000E+03   TIME STEP NUMBER             679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000881E+04
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 :  0.23763E+00 0.12219E+01
   Friction velocity        uet   :  0.14213E-01 0.72568E-01
   Friction velocity        uk    :  0.17282E-01 0.38756E-01
   Dimensionless distance   yplus :  0.42512E+03 0.95321E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59614E+01      59   0.13560E-02   0.19541E-01 
c  VelocityX    0.46297E+04      12   0.70121E-02   0.42376E-03 
c  VelocityY    0.46297E+04      12   0.70121E-02   0.27627E-04 
c  VelocityZ    0.46297E+04      12   0.70121E-02   0.53048E-04 
c  TurbEner     0.59779E+01      13   0.13320E-03   0.14826E-08 
c  Dissip       0.15049E+01      16   0.19912E-02   0.43499E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.13           54548           26775           27269
v  Velocity[x]            0.29278          2.0147         0.90807         0.90984
v  Velocity[y]            -0.3669         0.70165      0.00055186      0.00032901
v  Velocity[z]           -0.41985         0.50572      -0.0012628      -0.0013801
v  TurbEner            0.00099869        0.015331       0.0032854       0.0033453
v  Dissip              9.2105e-05        0.032252      0.00045208      0.00039087
v  TurbVisc               0.16292          11.328           4.711          5.2722
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              679:        0.89518E-01

===============================================================


 INSTANT    0.680000000E+03   TIME STEP NUMBER             680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001672E+04
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 :  0.23773E+00 0.13250E+01
   Friction velocity        uet   :  0.14220E-01 0.78974E-01
   Friction velocity        uk    :  0.17309E-01 0.38773E-01
   Dimensionless distance   yplus :  0.42490E+03 0.95322E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60410E+01      57   0.15445E-02   0.19793E-01 
c  VelocityX    0.46298E+04      12   0.68139E-02   0.33063E-03 
c  VelocityY    0.46298E+04      12   0.68139E-02   0.27030E-04 
c  VelocityZ    0.46298E+04      12   0.68139E-02   0.47880E-04 
c  TurbEner     0.59774E+01      13   0.12676E-03   0.17347E-08 
c  Dissip       0.14670E+01      16   0.22621E-02   0.73206E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.27           54539           26775           27269
v  Velocity[x]            0.29295          2.0902         0.90807         0.90984
v  Velocity[y]           -0.38284         0.69503      0.00054977      0.00033042
v  Velocity[z]           -0.42043         0.51044      -0.0012456      -0.0013671
v  TurbEner             0.0010001        0.014777       0.0032856       0.0033455
v  Dissip              9.2054e-05        0.030811      0.00045189      0.00039075
v  TurbVisc               0.16297          11.318           4.711          5.2722
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              680:        0.89375E-01

===============================================================


 INSTANT    0.681000000E+03   TIME STEP NUMBER             681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000043E+04
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 :  0.23762E+00 0.12146E+01
   Friction velocity        uet   :  0.14214E-01 0.72349E-01
   Friction velocity        uk    :  0.17321E-01 0.38792E-01
   Dimensionless distance   yplus :  0.42554E+03 0.95322E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62910E+01      68   0.14836E-02   0.20641E-01 
c  VelocityX    0.46299E+04      13   0.69330E-02   0.39761E-03 
c  VelocityY    0.46299E+04      13   0.69330E-02   0.30059E-04 
c  VelocityZ    0.46299E+04      13   0.69330E-02   0.60276E-04 
c  TurbEner     0.59778E+01      13   0.74365E-04   0.12194E-08 
c  Dissip       0.14678E+01      14   0.55806E-03   0.41954E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.54           54514           26776           27270
v  Velocity[x]            0.29243          2.1407         0.90807         0.90985
v  Velocity[y]           -0.36738         0.70247      0.00055426      0.00033411
v  Velocity[z]           -0.42209         0.50439      -0.0012551       -0.001372
v  TurbEner            0.00099884        0.014687       0.0032857       0.0033456
v  Dissip              9.2064e-05        0.030449      0.00045186      0.00039073
v  TurbVisc               0.16336          11.348          4.7112          5.2724
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              681:        0.92546E-01

===============================================================


 INSTANT    0.682000000E+03   TIME STEP NUMBER             682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998947E+04
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 :  0.23767E+00 0.13255E+01
   Friction velocity        uet   :  0.14217E-01 0.79013E-01
   Friction velocity        uk    :  0.17310E-01 0.38817E-01
   Dimensionless distance   yplus :  0.42559E+03 0.95310E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.80746E+01      60   0.14548E-02   0.26462E-01 
c  VelocityX    0.46299E+04      12   0.73119E-02   0.42293E-03 
c  VelocityY    0.46299E+04      12   0.73119E-02   0.58843E-04 
c  VelocityZ    0.46299E+04      12   0.73119E-02   0.10020E-03 
c  TurbEner     0.59783E+01      13   0.72664E-04   0.11369E-08 
c  Dissip       0.14889E+01      15   0.71245E-03   0.12634E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.89           54530           26776           27270
v  Velocity[x]            0.29264          2.1869         0.90804         0.90982
v  Velocity[y]            -0.3823         0.69179      0.00056443      0.00034405
v  Velocity[z]           -0.42096         0.51184       -0.001237      -0.0013587
v  TurbEner             0.0010013         0.01481       0.0032859       0.0033457
v  Dissip               9.206e-05        0.030599      0.00045202      0.00039083
v  TurbVisc               0.16331          11.392          4.7113          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              682:        0.89654E-01

===============================================================


 INSTANT    0.683000000E+03   TIME STEP NUMBER             683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999279E+04
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 :  0.23798E+00 0.12171E+01
   Friction velocity        uet   :  0.14236E-01 0.72550E-01
   Friction velocity        uk    :  0.17332E-01 0.38817E-01
   Dimensionless distance   yplus :  0.42520E+03 0.95295E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.74045E+01      59   0.15010E-02   0.24256E-01 
c  VelocityX    0.46297E+04      12   0.64782E-02   0.44882E-03 
c  VelocityY    0.46297E+04      12   0.64782E-02   0.70902E-04 
c  VelocityZ    0.46297E+04      12   0.64782E-02   0.51001E-04 
c  TurbEner     0.59786E+01      14   0.14951E-03   0.20933E-08 
c  Dissip       0.14947E+01      16   0.19701E-02   0.42469E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.08           54531           26775           27270
v  Velocity[x]            0.29328          2.0063         0.90806         0.90984
v  Velocity[y]           -0.36617         0.69921      0.00055172      0.00032993
v  Velocity[z]           -0.42037         0.50639      -0.0012524      -0.0013716
v  TurbEner             0.0010042        0.015505        0.003286       0.0033458
v  Dissip              9.2065e-05        0.032128       0.0004522      0.00039096
v  TurbVisc               0.16314          11.382          4.7114          5.2725
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              683:        0.90929E-01

===============================================================


 INSTANT    0.684000000E+03   TIME STEP NUMBER             684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000624E+04
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 :  0.23772E+00 0.13235E+01
   Friction velocity        uet   :  0.14220E-01 0.78892E-01
   Friction velocity        uk    :  0.17357E-01 0.38795E-01
   Dimensionless distance   yplus :  0.42628E+03 0.95283E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58847E+01      56   0.12592E-02   0.19308E-01 
c  VelocityX    0.46299E+04      12   0.66238E-02   0.33021E-03 
c  VelocityY    0.46299E+04      12   0.66238E-02   0.37378E-04 
c  VelocityZ    0.46299E+04      12   0.66238E-02   0.29841E-04 
c  TurbEner     0.59779E+01      13   0.13038E-03   0.17406E-08 
c  Dissip       0.14649E+01      16   0.21598E-02   0.64142E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.58           54541           26776           27270
v  Velocity[x]            0.29279          2.0983         0.90804         0.90982
v  Velocity[y]           -0.38232         0.69224      0.00054769      0.00032903
v  Velocity[z]           -0.42252         0.51103      -0.0012535      -0.0013739
v  TurbEner             0.0010017        0.014911        0.003286       0.0033458
v  Dissip               9.211e-05        0.030675      0.00045198      0.00039081
v  TurbVisc               0.16372          11.318          4.7114          5.2725
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              684:        0.89708E-01

===============================================================


 INSTANT    0.685000000E+03   TIME STEP NUMBER             685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997694E+04
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 :  0.23757E+00 0.12155E+01
   Friction velocity        uet   :  0.14211E-01 0.72460E-01
   Friction velocity        uk    :  0.17335E-01 0.38690E-01
   Dimensionless distance   yplus :  0.42604E+03 0.95251E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63635E+01      52   0.12608E-02   0.20853E-01 
c  VelocityX    0.46298E+04      13   0.71311E-02   0.28700E-03 
c  VelocityY    0.46298E+04      13   0.71311E-02   0.32451E-04 
c  VelocityZ    0.46298E+04      13   0.71311E-02   0.42168E-04 
c  TurbEner     0.59782E+01      12   0.55918E-04   0.59982E-09 
c  Dissip       0.14701E+01      13   0.30884E-03   0.21163E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.19           54550           26776           27270
v  Velocity[x]            0.29247          2.1367         0.90805         0.90983
v  Velocity[y]           -0.36779         0.70152      0.00054744      0.00032611
v  Velocity[z]           -0.42052         0.50411      -0.0012579       -0.001376
v  TurbEner             0.0010055        0.014909       0.0032859       0.0033457
v  Dissip              9.2128e-05        0.030563      0.00045195      0.00039078
v  TurbVisc               0.16348          11.311          4.7114          5.2726
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              685:        0.88940E-01

===============================================================


 INSTANT    0.686000000E+03   TIME STEP NUMBER             686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000687E+04
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 :  0.23755E+00 0.13235E+01
   Friction velocity        uet   :  0.14209E-01 0.78889E-01
   Friction velocity        uk    :  0.17368E-01 0.38630E-01
   Dimensionless distance   yplus :  0.42610E+03 0.95228E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61276E+01      59   0.14532E-02   0.20086E-01 
c  VelocityX    0.46299E+04      12   0.74546E-02   0.37692E-03 
c  VelocityY    0.46299E+04      12   0.74546E-02   0.33420E-04 
c  VelocityZ    0.46299E+04      12   0.74546E-02   0.43409E-04 
c  TurbEner     0.59797E+01      13   0.75902E-04   0.89076E-09 
c  Dissip       0.14928E+01      15   0.78063E-03   0.13650E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.51           54540           26776           27271
v  Velocity[x]            0.29277          2.1761         0.90806         0.90984
v  Velocity[y]            -0.3826         0.69425      0.00054859      0.00033002
v  Velocity[z]           -0.41962          0.5117      -0.0012428      -0.0013647
v  TurbEner             0.0010072        0.015068       0.0032863        0.003346
v  Dissip              9.2104e-05        0.030914       0.0004522      0.00039095
v  TurbVisc               0.16354          11.335          4.7114          5.2726
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              686:        0.89581E-01

===============================================================


 INSTANT    0.687000000E+03   TIME STEP NUMBER             687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999987E+04
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 :  0.23758E+00 0.12166E+01
   Friction velocity        uet   :  0.14211E-01 0.72527E-01
   Friction velocity        uk    :  0.17383E-01 0.38717E-01
   Dimensionless distance   yplus :  0.42693E+03 0.95233E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66657E+01      58   0.15993E-02   0.21852E-01 
c  VelocityX    0.46299E+04      12   0.68602E-02   0.42114E-03 
c  VelocityY    0.46299E+04      12   0.68602E-02   0.34475E-04 
c  VelocityZ    0.46299E+04      12   0.68602E-02   0.53086E-04 
c  TurbEner     0.59808E+01      13   0.82700E-04   0.12683E-08 
c  Dissip       0.15168E+01      15   0.90671E-03   0.17263E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.78           54515           26776           27270
v  Velocity[x]            0.29297          2.1948         0.90808         0.90986
v  Velocity[y]           -0.36773         0.70082      0.00055074      0.00033218
v  Velocity[z]           -0.42029         0.50726      -0.0012496      -0.0013659
v  TurbEner             0.0010055        0.015279       0.0032865       0.0033462
v  Dissip              9.2107e-05        0.031417      0.00045247      0.00039114
v  TurbVisc               0.16398           11.38          4.7116          5.2727
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              687:        0.89624E-01

===============================================================


 INSTANT    0.688000000E+03   TIME STEP NUMBER             688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001666E+04
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 :  0.23793E+00 0.13256E+01
   Friction velocity        uet   :  0.14232E-01 0.79017E-01
   Friction velocity        uk    :  0.17368E-01 0.38780E-01
   Dimensionless distance   yplus :  0.42696E+03 0.95234E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72205E+01      55   0.15899E-02   0.23674E-01 
c  VelocityX    0.46299E+04      12   0.67581E-02   0.39612E-03 
c  VelocityY    0.46299E+04      12   0.67581E-02   0.32097E-04 
c  VelocityZ    0.46299E+04      12   0.67581E-02   0.96560E-04 
c  TurbEner     0.59812E+01      13   0.12393E-03   0.15481E-08 
c  Dissip       0.15408E+01      16   0.21662E-02   0.55247E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.42           54521           26776           27270
v  Velocity[x]            0.29266          2.0421         0.90806         0.90983
v  Velocity[y]           -0.38298         0.69461      0.00055557      0.00033665
v  Velocity[z]           -0.42101         0.51349      -0.0012426      -0.0013638
v  TurbEner             0.0010078        0.015894       0.0032868       0.0033464
v  Dissip              9.2115e-05        0.033164      0.00045281      0.00039137
v  TurbVisc               0.16389          11.369          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              688:        0.89497E-01

===============================================================


 INSTANT    0.689000000E+03   TIME STEP NUMBER             689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998136E+04
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 :  0.23789E+00 0.12186E+01
   Friction velocity        uet   :  0.14229E-01 0.72293E-01
   Friction velocity        uk    :  0.17388E-01 0.38780E-01
   Dimensionless distance   yplus :  0.42658E+03 0.95256E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67261E+01      54   0.14043E-02   0.22040E-01 
c  VelocityX    0.46297E+04      12   0.71477E-02   0.52236E-03 
c  VelocityY    0.46297E+04      12   0.71477E-02   0.24876E-04 
c  VelocityZ    0.46297E+04      12   0.71477E-02   0.64114E-04 
c  TurbEner     0.59792E+01      13   0.10821E-03   0.17610E-08 
c  Dissip       0.14956E+01      16   0.14421E-02   0.52218E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.05           54522           26776           27270
v  Velocity[x]            0.29302          1.7281         0.90804         0.90981
v  Velocity[y]           -0.36728         0.70334      0.00054868      0.00032811
v  Velocity[z]           -0.42143         0.50707      -0.0012564      -0.0013746
v  TurbEner             0.0010109        0.015815       0.0032866       0.0033463
v  Dissip              9.2125e-05        0.033224       0.0004526      0.00039124
v  TurbVisc               0.16376          11.375          4.7117          5.2729
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              689:        0.89467E-01

===============================================================


 INSTANT    0.690000000E+03   TIME STEP NUMBER             690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000447E+04
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 :  0.23747E+00 0.13255E+01
   Friction velocity        uet   :  0.14203E-01 0.79009E-01
   Friction velocity        uk    :  0.17415E-01 0.38744E-01
   Dimensionless distance   yplus :  0.42776E+03 0.95292E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58751E+01      61   0.14039E-02   0.19286E-01 
c  VelocityX    0.46298E+04      12   0.61903E-02   0.36648E-03 
c  VelocityY    0.46298E+04      12   0.61903E-02   0.29928E-04 
c  VelocityZ    0.46298E+04      12   0.61903E-02   0.34001E-04 
c  TurbEner     0.59744E+01      15   0.40994E-03   0.91267E-08 
c  Dissip       0.13500E+01      18   0.81048E-02   0.48070E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.79           54505           26777           27271
v  Velocity[x]            0.29261          1.8824         0.90804         0.90982
v  Velocity[y]           -0.38344         0.69306      0.00055574      0.00033627
v  Velocity[z]           -0.42028         0.51127      -0.0012493      -0.0013677
v  TurbEner              0.001008        0.013577       0.0032863        0.003346
v  Dissip              9.2139e-05        0.027541      0.00045192      0.00039073
v  TurbVisc               0.16444          11.349          4.7118           5.273
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              690:        0.90783E-01

===============================================================


 INSTANT    0.691000000E+03   TIME STEP NUMBER             691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998407E+04
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 :  0.23776E+00 0.12177E+01
   Friction velocity        uet   :  0.14221E-01 0.72580E-01
   Friction velocity        uk    :  0.17390E-01 0.38652E-01
   Dimensionless distance   yplus :  0.42744E+03 0.95288E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62114E+01      54   0.12502E-02   0.20370E-01 
c  VelocityX    0.46298E+04      12   0.69012E-02   0.29348E-03 
c  VelocityY    0.46298E+04      12   0.69012E-02   0.34598E-04 
c  VelocityZ    0.46298E+04      12   0.69012E-02   0.31535E-04 
c  TurbEner     0.59721E+01      14   0.15988E-03   0.27345E-08 
c  Dissip       0.12910E+01      18   0.37062E-02   0.13237E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.09           54518           26777           27271
v  Velocity[x]            0.29268           1.991         0.90804         0.90981
v  Velocity[y]           -0.36804         0.70063       0.0005529      0.00033212
v  Velocity[z]           -0.42117         0.50489      -0.0012564      -0.0013754
v  TurbEner             0.0010114        0.012855       0.0032858       0.0033456
v  Dissip              9.2181e-05        0.025182      0.00045116      0.00039017
v  TurbVisc               0.16422          11.347          4.7118          5.2731
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              691:        0.89660E-01

===============================================================


 INSTANT    0.692000000E+03   TIME STEP NUMBER             692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999579E+04
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 :  0.23768E+00 0.13243E+01
   Friction velocity        uet   :  0.14215E-01 0.78939E-01
   Friction velocity        uk    :  0.17419E-01 0.38682E-01
   Dimensionless distance   yplus :  0.42737E+03 0.95284E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63945E+01      69   0.12922E-02   0.20943E-01 
c  VelocityX    0.46299E+04      12   0.69783E-02   0.35031E-03 
c  VelocityY    0.46299E+04      12   0.69783E-02   0.29268E-04 
c  VelocityZ    0.46299E+04      12   0.69783E-02   0.29969E-04 
c  TurbEner     0.59718E+01      13   0.83322E-04   0.12037E-08 
c  Dissip       0.12648E+01      17   0.19961E-02   0.61386E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.02           54532           26776           27270
v  Velocity[x]            0.29306          2.0786         0.90803         0.90981
v  Velocity[y]            -0.3826         0.69565      0.00054669      0.00032732
v  Velocity[z]           -0.41803         0.51234      -0.0012468      -0.0013671
v  TurbEner             0.0010124         0.01275       0.0032854       0.0033453
v  Dissip              9.2196e-05        0.024283       0.0004505       0.0003897
v  TurbVisc               0.16427          11.323          4.7119          5.2731
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              692:        0.92495E-01

===============================================================


 INSTANT    0.693000000E+03   TIME STEP NUMBER             693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000920E+04
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 :  0.23755E+00 0.12136E+01
   Friction velocity        uet   :  0.14208E-01 0.72346E-01
   Friction velocity        uk    :  0.17428E-01 0.38775E-01
   Dimensionless distance   yplus :  0.42799E+03 0.95309E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58256E+01      60   0.12514E-02   0.19105E-01 
c  VelocityX    0.46299E+04      13   0.70490E-02   0.31593E-03 
c  VelocityY    0.46299E+04      13   0.70490E-02   0.27936E-04 
c  VelocityZ    0.46299E+04      13   0.70490E-02   0.80410E-04 
c  TurbEner     0.59720E+01      13   0.75435E-04   0.84861E-09 
c  Dissip       0.12552E+01      17   0.10709E-02   0.24342E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.28           54542           26776           27270
v  Velocity[x]            0.29261          2.1242         0.90805         0.90983
v  Velocity[y]           -0.36627         0.70476      0.00054918      0.00032614
v  Velocity[z]            -0.4203         0.50684       -0.001252      -0.0013698
v  TurbEner             0.0010109         0.01299        0.003285        0.003345
v  Dissip              9.2166e-05        0.024151      0.00044987      0.00038925
v  TurbVisc               0.16468          11.316           4.712          5.2733
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              693:        0.90524E-01

===============================================================


 INSTANT    0.694000000E+03   TIME STEP NUMBER             694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001050E+04
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 :  0.23787E+00 0.13252E+01
   Friction velocity        uet   :  0.14227E-01 0.78994E-01
   Friction velocity        uk    :  0.17415E-01 0.38791E-01
   Dimensionless distance   yplus :  0.42811E+03 0.95307E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61650E+01      52   0.13774E-02   0.20216E-01 
c  VelocityX    0.46299E+04      13   0.70657E-02   0.38064E-03 
c  VelocityY    0.46299E+04      13   0.70657E-02   0.23042E-04 
c  VelocityZ    0.46299E+04      13   0.70657E-02   0.60710E-04 
c  TurbEner     0.59728E+01      13   0.13286E-03   0.15509E-08 
c  Dissip       0.12530E+01      16   0.16987E-02   0.29127E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.97           54549           26776           27270
v  Velocity[x]            0.29262          1.9788         0.90805         0.90983
v  Velocity[y]           -0.38258          0.6924      0.00054971      0.00032814
v  Velocity[z]            -0.4227         0.51124      -0.0012603      -0.0013795
v  TurbEner             0.0010131        0.013696       0.0032851       0.0033451
v  Dissip              9.2159e-05        0.025312      0.00044952      0.00038902
v  TurbVisc               0.16473          11.343          4.7122          5.2734
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              694:        0.88451E-01

===============================================================


 INSTANT    0.695000000E+03   TIME STEP NUMBER             695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998804E+04
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 :  0.23788E+00 0.12184E+01
   Friction velocity        uet   :  0.14227E-01 0.72615E-01
   Friction velocity        uk    :  0.17433E-01 0.38786E-01
   Dimensionless distance   yplus :  0.42774E+03 0.95323E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60508E+01      54   0.14276E-02   0.19838E-01 
c  VelocityX    0.46299E+04      12   0.68815E-02   0.38228E-03 
c  VelocityY    0.46299E+04      12   0.68815E-02   0.26155E-04 
c  VelocityZ    0.46299E+04      12   0.68815E-02   0.44582E-04 
c  TurbEner     0.59725E+01      13   0.10429E-03   0.13632E-08 
c  Dissip       0.12249E+01      17   0.20719E-02   0.55576E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.28           54542           26776           27270
v  Velocity[x]            0.29302          2.0657         0.90806         0.90983
v  Velocity[y]           -0.36823         0.70076       0.0005491      0.00032761
v  Velocity[z]            -0.4204          0.5041      -0.0012568      -0.0013723
v  TurbEner             0.0010156         0.01327       0.0032851       0.0033451
v  Dissip              9.2163e-05        0.024068      0.00044895      0.00038863
v  TurbVisc               0.16463           11.39          4.7125          5.2737
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              695:        0.89218E-01

===============================================================


 INSTANT    0.696000000E+03   TIME STEP NUMBER             696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001447E+04
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 :  0.23794E+00 0.13243E+01
   Friction velocity        uet   :  0.14230E-01 0.78932E-01
   Friction velocity        uk    :  0.17455E-01 0.38781E-01
   Dimensionless distance   yplus :  0.42885E+03 0.95303E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64783E+01      62   0.15666E-02   0.21253E-01 
c  VelocityX    0.46300E+04      12   0.74422E-02   0.42494E-03 
c  VelocityY    0.46300E+04      12   0.74422E-02   0.27492E-04 
c  VelocityZ    0.46300E+04      12   0.74422E-02   0.33057E-04 
c  TurbEner     0.59736E+01      13   0.75913E-04   0.11175E-08 
c  Dissip       0.12289E+01      15   0.38157E-03   0.43385E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.7           54517           26777           27271
v  Velocity[x]            0.29255          2.1271         0.90806         0.90984
v  Velocity[y]           -0.38265         0.69403      0.00055093      0.00033333
v  Velocity[z]           -0.42148         0.51174      -0.0012545      -0.0013721
v  TurbEner             0.0010116        0.013362       0.0032852       0.0033452
v  Dissip                9.21e-05        0.023968      0.00044864      0.00038842
v  TurbVisc                0.1653           11.38          4.7128           5.274
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              696:        0.90373E-01

===============================================================


 INSTANT    0.697000000E+03   TIME STEP NUMBER             697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998036E+04
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 :  0.23775E+00 0.12172E+01
   Friction velocity        uet   :  0.14220E-01 0.72557E-01
   Friction velocity        uk    :  0.17420E-01 0.38711E-01
   Dimensionless distance   yplus :  0.42841E+03 0.95301E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62516E+01      54   0.11987E-02   0.20493E-01 
c  VelocityX    0.46301E+04      12   0.72060E-02   0.39108E-03 
c  VelocityY    0.46301E+04      12   0.72060E-02   0.44859E-04 
c  VelocityZ    0.46301E+04      12   0.72060E-02   0.30733E-04 
c  TurbEner     0.59743E+01      13   0.95251E-04   0.17546E-08 
c  Dissip       0.12490E+01      16   0.97511E-03   0.18433E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.41           54525           26777           27271
v  Velocity[x]            0.29277          2.1532         0.90806         0.90983
v  Velocity[y]           -0.36827         0.70218      0.00055265      0.00033236
v  Velocity[z]           -0.42217         0.50695      -0.0012583      -0.0013757
v  TurbEner             0.0010139        0.013719       0.0032854       0.0033453
v  Dissip              9.2083e-05        0.024441      0.00044857      0.00038837
v  TurbVisc               0.16503           11.33          4.7132          5.2744
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              697:        0.89602E-01

===============================================================


 INSTANT    0.698000000E+03   TIME STEP NUMBER             698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000101E+04
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 :  0.23770E+00 0.13235E+01
   Friction velocity        uet   :  0.14217E-01 0.78886E-01
   Friction velocity        uk    :  0.17440E-01 0.38769E-01
   Dimensionless distance   yplus :  0.42814E+03 0.95281E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61919E+01      60   0.14116E-02   0.20288E-01 
c  VelocityX    0.46301E+04      12   0.73216E-02   0.38361E-03 
c  VelocityY    0.46301E+04      12   0.73216E-02   0.22596E-04 
c  VelocityZ    0.46301E+04      12   0.73216E-02   0.60597E-04 
c  TurbEner     0.59758E+01      14   0.14781E-03   0.23222E-08 
c  Dissip       0.12683E+01      17   0.21368E-02   0.49725E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.31           54525           26777           27271
v  Velocity[x]             0.2928          1.9987         0.90806         0.90983
v  Velocity[y]           -0.38302         0.69508      0.00055592      0.00033542
v  Velocity[z]           -0.41928         0.51364      -0.0012537      -0.0013732
v  TurbEner              0.001014        0.014509       0.0032857       0.0033455
v  Dissip              9.2046e-05        0.026036      0.00044866      0.00038844
v  TurbVisc               0.16501          11.321          4.7135          5.2747
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              698:        0.89819E-01

===============================================================


 INSTANT    0.699000000E+03   TIME STEP NUMBER             699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999223E+04
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 :  0.23739E+00 0.12169E+01
   Friction velocity        uet   :  0.14199E-01 0.72540E-01
   Friction velocity        uk    :  0.17441E-01 0.38808E-01
   Dimensionless distance   yplus :  0.42862E+03 0.95250E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67391E+01      61   0.15039E-02   0.22106E-01 
c  VelocityX    0.46302E+04      12   0.66497E-02   0.35920E-03 
c  VelocityY    0.46302E+04      12   0.66497E-02   0.27668E-04 
c  VelocityZ    0.46302E+04      12   0.66497E-02   0.87229E-04 
c  TurbEner     0.59753E+01      13   0.98215E-04   0.13637E-08 
c  Dissip       0.12521E+01      16   0.16093E-02   0.33253E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.81           54513           26777           27272
v  Velocity[x]            0.29288          2.0835         0.90808         0.90985
v  Velocity[y]           -0.36671         0.70122       0.0005609      0.00033803
v  Velocity[z]              -0.42          0.5078       -0.001245      -0.0013622
v  TurbEner             0.0010112         0.01405       0.0032857       0.0033456
v  Dissip               9.206e-05        0.024971      0.00044845       0.0003883
v  TurbVisc                0.1654          11.348          4.7138           5.275
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              699:        0.90340E-01

===============================================================


 INSTANT    0.700000000E+03   TIME STEP NUMBER             700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998469E+04
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 :  0.23768E+00 0.13253E+01
   Friction velocity        uet   :  0.14217E-01 0.78995E-01
   Friction velocity        uk    :  0.17418E-01 0.38804E-01
   Dimensionless distance   yplus :  0.42840E+03 0.95228E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62144E+01      54   0.13193E-02   0.20372E-01 
c  VelocityX    0.46302E+04      12   0.68101E-02   0.35098E-03 
c  VelocityY    0.46302E+04      12   0.68101E-02   0.29228E-04 
c  VelocityZ    0.46302E+04      12   0.68101E-02   0.33648E-04 
c  TurbEner     0.59756E+01      13   0.65762E-04   0.11224E-08 
c  Dissip       0.12634E+01      15   0.39486E-03   0.42156E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.35           54519           26778           27272
v  Velocity[x]            0.29287          2.1301         0.90805         0.90984
v  Velocity[y]           -0.38283         0.69424      0.00055899      0.00033708
v  Velocity[z]           -0.42069         0.51201       -0.001238      -0.0013582
v  TurbEner             0.0010124        0.014169       0.0032858       0.0033457
v  Dissip              9.2049e-05         0.02512      0.00044845       0.0003883
v  TurbVisc               0.16533          11.332          4.7141          5.2752
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              700:        0.89415E-01

===============================================================


 INSTANT    0.701000000E+03   TIME STEP NUMBER             701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998827E+04
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 :  0.23811E+00 0.12134E+01
   Friction velocity        uet   :  0.14243E-01 0.72328E-01
   Friction velocity        uk    :  0.17428E-01 0.38660E-01
   Dimensionless distance   yplus :  0.42774E+03 0.95247E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61220E+01      55   0.12820E-02   0.20081E-01 
c  VelocityX    0.46303E+04      12   0.62860E-02   0.31976E-03 
c  VelocityY    0.46303E+04      12   0.62860E-02   0.24491E-04 
c  VelocityZ    0.46303E+04      12   0.62860E-02   0.44158E-04 
c  TurbEner     0.59769E+01      13   0.85138E-04   0.12367E-08 
c  Dissip       0.12919E+01      16   0.11990E-02   0.30742E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.1           54533           26778           27272
v  Velocity[x]             0.2931          2.1804         0.90805         0.90983
v  Velocity[y]           -0.36844         0.70247      0.00055463         0.00033
v  Velocity[z]           -0.42045         0.50467       -0.001249       -0.001366
v  TurbEner             0.0010144        0.014366        0.003286       0.0033458
v  Dissip              9.2114e-05        0.025661      0.00044866      0.00038843
v  TurbVisc               0.16517          11.323          4.7144          5.2755
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              701:        0.89333E-01

===============================================================


 INSTANT    0.702000000E+03   TIME STEP NUMBER             702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000965E+04
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 :  0.23778E+00 0.13252E+01
   Friction velocity        uet   :  0.14224E-01 0.78991E-01
   Friction velocity        uk    :  0.17445E-01 0.38711E-01
   Dimensionless distance   yplus :  0.42862E+03 0.95261E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54589E+01      55   0.12641E-02   0.17901E-01 
c  VelocityX    0.46303E+04      13   0.69325E-02   0.27858E-03 
c  VelocityY    0.46303E+04      13   0.69325E-02   0.24150E-04 
c  VelocityZ    0.46303E+04      13   0.69325E-02   0.42255E-04 
c  TurbEner     0.59784E+01      13   0.96281E-04   0.12861E-08 
c  Dissip       0.13287E+01      16   0.15114E-02   0.38041E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.6           54545           26777           27272
v  Velocity[x]            0.29262          2.1951         0.90805         0.90984
v  Velocity[y]           -0.38317         0.69262      0.00054819      0.00032606
v  Velocity[z]           -0.42211          0.5119      -0.0012516      -0.0013702
v  TurbEner             0.0010114        0.014738       0.0032863        0.003346
v  Dissip               9.219e-05        0.026659      0.00044896      0.00038863
v  TurbVisc               0.16583          11.362          4.7146          5.2758
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              702:        0.89871E-01

===============================================================


 INSTANT    0.703000000E+03   TIME STEP NUMBER             703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001377E+04
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 :  0.23764E+00 0.12170E+01
   Friction velocity        uet   :  0.14216E-01 0.72541E-01
   Friction velocity        uk    :  0.17419E-01 0.38689E-01
   Dimensionless distance   yplus :  0.42824E+03 0.95259E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70770E+01      59   0.14065E-02   0.23203E-01 
c  VelocityX    0.46303E+04      12   0.70133E-02   0.37662E-03 
c  VelocityY    0.46303E+04      12   0.70133E-02   0.35551E-04 
c  VelocityZ    0.46303E+04      12   0.70133E-02   0.10743E-03 
c  TurbEner     0.59795E+01      13   0.13672E-03   0.18071E-08 
c  Dissip       0.13615E+01      17   0.25130E-02   0.77973E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.55           54551           26776           27271
v  Velocity[x]            0.29289          2.0302         0.90805         0.90982
v  Velocity[y]           -0.36838         0.70001      0.00056979      0.00034357
v  Velocity[z]           -0.42102         0.50725      -0.0012476      -0.0013675
v  TurbEner             0.0010155        0.015499       0.0032866       0.0033462
v  Dissip              9.2204e-05        0.028655       0.0004494      0.00038894
v  TurbVisc                0.1657          11.348          4.7149           5.276
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              703:        0.90126E-01

===============================================================


 INSTANT    0.704000000E+03   TIME STEP NUMBER             704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002280E+04
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 :  0.23793E+00 0.13244E+01
   Friction velocity        uet   :  0.14233E-01 0.78946E-01
   Friction velocity        uk    :  0.17454E-01 0.38720E-01
   Dimensionless distance   yplus :  0.42827E+03 0.95209E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65582E+01      67   0.14891E-02   0.21511E-01 
c  VelocityX    0.46303E+04      12   0.68649E-02   0.38319E-03 
c  VelocityY    0.46303E+04      12   0.68649E-02   0.46821E-04 
c  VelocityZ    0.46303E+04      12   0.68649E-02   0.53083E-04 
c  TurbEner     0.59792E+01      13   0.10834E-03   0.15365E-08 
c  Dissip       0.13499E+01      16   0.12443E-02   0.26168E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.07           54545           26778           27272
v  Velocity[x]            0.29302          2.0927         0.90807         0.90986
v  Velocity[y]           -0.38301         0.69316      0.00055178      0.00033151
v  Velocity[z]           -0.41962           0.514      -0.0012492      -0.0013674
v  TurbEner             0.0010177        0.015004        0.003287       0.0033465
v  Dissip              9.2159e-05         0.02786       0.0004495      0.00038901
v  TurbVisc               0.16591          11.356          4.7152          5.2762
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              704:        0.91213E-01

===============================================================


 INSTANT    0.705000000E+03   TIME STEP NUMBER             705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998410E+04
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 :  0.23728E+00 0.12330E+01
   Friction velocity        uet   :  0.14194E-01 0.72539E-01
   Friction velocity        uk    :  0.17473E-01 0.38722E-01
   Dimensionless distance   yplus :  0.42911E+03 0.95286E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64430E+01      54   0.15228E-02   0.21135E-01 
c  VelocityX    0.46304E+04      12   0.63402E-02   0.37367E-03 
c  VelocityY    0.46304E+04      12   0.63402E-02   0.32810E-04 
c  VelocityZ    0.46304E+04      12   0.63402E-02   0.28215E-04 
c  TurbEner     0.59800E+01      13   0.63531E-04   0.99605E-09 
c  Dissip       0.13681E+01      15   0.50010E-03   0.75798E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.22           54522           26778           27272
v  Velocity[x]            0.29252          2.1551         0.90805         0.90983
v  Velocity[y]           -0.36681         0.70204      0.00056078       0.0003386
v  Velocity[z]           -0.42038         0.50804      -0.0012397      -0.0013569
v  TurbEner             0.0010171        0.014929       0.0032873       0.0033467
v  Dissip              9.2176e-05        0.027977      0.00044976      0.00038919
v  TurbVisc               0.16652          11.335          4.7154          5.2765
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              705:        0.88962E-01

===============================================================


 INSTANT    0.706000000E+03   TIME STEP NUMBER             706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998810E+04
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 :  0.23792E+00 0.13238E+01
   Friction velocity        uet   :  0.14233E-01 0.78909E-01
   Friction velocity        uk    :  0.17468E-01 0.38765E-01
   Dimensionless distance   yplus :  0.42934E+03 0.95353E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57989E+01      56   0.12402E-02   0.19021E-01 
c  VelocityX    0.46304E+04      12   0.73257E-02   0.31915E-03 
c  VelocityY    0.46304E+04      12   0.73257E-02   0.28137E-04 
c  VelocityZ    0.46304E+04      12   0.73257E-02   0.44174E-04 
c  TurbEner     0.59806E+01      13   0.79118E-04   0.11779E-08 
c  Dissip       0.13982E+01      16   0.11458E-02   0.28518E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.41           54531           26779           27273
v  Velocity[x]             0.2926          2.1744         0.90804         0.90982
v  Velocity[y]           -0.38277         0.69492      0.00055099       0.0003327
v  Velocity[z]            -0.4212         0.51224      -0.0012498        -0.00137
v  TurbEner             0.0010203        0.015112       0.0032876        0.003347
v  Dissip              9.2171e-05        0.028595      0.00045016      0.00038945
v  TurbVisc               0.16668          11.333          4.7156          5.2767
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              706:        0.89792E-01

===============================================================


 INSTANT    0.707000000E+03   TIME STEP NUMBER             707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997865E+04
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 :  0.23801E+00 0.12169E+01
   Friction velocity        uet   :  0.14238E-01 0.72542E-01
   Friction velocity        uk    :  0.17496E-01 0.38785E-01
   Dimensionless distance   yplus :  0.42909E+03 0.95353E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67029E+01      56   0.13862E-02   0.21973E-01 
c  VelocityX    0.46304E+04      12   0.72307E-02   0.42478E-03 
c  VelocityY    0.46304E+04      12   0.72307E-02   0.20660E-04 
c  VelocityZ    0.46304E+04      12   0.72307E-02   0.11245E-03 
c  TurbEner     0.59811E+01      13   0.12315E-03   0.14748E-08 
c  Dissip       0.14209E+01      16   0.22150E-02   0.59946E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.9           54527           26778           27273
v  Velocity[x]            0.29329          2.0128         0.90804         0.90982
v  Velocity[y]           -0.36821         0.70134      0.00055846      0.00033641
v  Velocity[z]           -0.42225         0.50489       -0.001253      -0.0013715
v  TurbEner             0.0010246        0.015761       0.0032879       0.0033472
v  Dissip              9.2138e-05         0.03036      0.00045061      0.00038977
v  TurbVisc               0.16672          11.358          4.7159          5.2769
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              707:        0.89678E-01

===============================================================


 INSTANT    0.708000000E+03   TIME STEP NUMBER             708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999683E+04
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 :  0.23746E+00 0.13263E+01
   Friction velocity        uet   :  0.14205E-01 0.79056E-01
   Friction velocity        uk    :  0.17533E-01 0.38826E-01
   Dimensionless distance   yplus :  0.43048E+03 0.95365E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72030E+01      57   0.15815E-02   0.23632E-01 
c  VelocityX    0.46304E+04      13   0.67779E-02   0.41705E-03 
c  VelocityY    0.46304E+04      13   0.67779E-02   0.36951E-04 
c  VelocityZ    0.46304E+04      13   0.67779E-02   0.48606E-04 
c  TurbEner     0.59801E+01      13   0.12752E-03   0.17869E-08 
c  Dissip       0.13979E+01      16   0.17780E-02   0.45804E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.71           54510           26779           27274
v  Velocity[x]            0.29289          2.0797         0.90808         0.90986
v  Velocity[y]           -0.38277         0.69464      0.00054624      0.00032672
v  Velocity[z]           -0.42085         0.51223      -0.0012458      -0.0013643
v  TurbEner              0.001023        0.015118        0.003288       0.0033473
v  Dissip                9.21e-05         0.02913      0.00045062      0.00038977
v  TurbVisc               0.16762          11.341           4.716           5.277
v  total_pressure           83077      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              708:        0.90534E-01

===============================================================


 INSTANT    0.709000000E+03   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998164E+04
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 :  0.23800E+00 0.12320E+01
   Friction velocity        uet   :  0.14238E-01 0.72321E-01
   Friction velocity        uk    :  0.17519E-01 0.38754E-01
   Dimensionless distance   yplus :  0.43043E+03 0.95362E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65242E+01      56   0.12844E-02   0.21382E-01 
c  VelocityX    0.46305E+04      12   0.70400E-02   0.38213E-03 
c  VelocityY    0.46305E+04      12   0.70400E-02   0.39614E-04 
c  VelocityZ    0.46305E+04      12   0.70400E-02   0.28280E-04 
c  TurbEner     0.59802E+01      13   0.73523E-04   0.12058E-08 
c  Dissip       0.14076E+01      14   0.31840E-03   0.30262E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.83           54518           26779           27273
v  Velocity[x]            0.29253          2.1453         0.90806         0.90983
v  Velocity[y]            -0.3668         0.70319      0.00055848      0.00033513
v  Velocity[z]           -0.42204         0.50634      -0.0012549      -0.0013741
v  TurbEner              0.001028        0.014976       0.0032882       0.0033474
v  Dissip              9.2067e-05        0.029023      0.00045079      0.00038987
v  TurbVisc               0.16762          11.352          4.7161          5.2772
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              709:        0.89543E-01

===============================================================


 INSTANT    0.710000000E+03   TIME STEP NUMBER             710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001093E+04
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 :  0.23771E+00 0.13255E+01
   Friction velocity        uet   :  0.14220E-01 0.79010E-01
   Friction velocity        uk    :  0.17561E-01 0.38769E-01
   Dimensionless distance   yplus :  0.43064E+03 0.95328E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72509E+01      56   0.16634E-02   0.23760E-01 
c  VelocityX    0.46305E+04      12   0.73668E-02   0.38913E-03 
c  VelocityY    0.46305E+04      12   0.73668E-02   0.36122E-04 
c  VelocityZ    0.46305E+04      12   0.73668E-02   0.46869E-04 
c  TurbEner     0.59811E+01      13   0.83441E-04   0.11435E-08 
c  Dissip       0.14323E+01      15   0.88770E-03   0.17449E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.24           54523           26779           27273
v  Velocity[x]            0.29288          2.1718         0.90807         0.90985
v  Velocity[y]            -0.3825         0.69269      0.00053985      0.00032112
v  Velocity[z]           -0.41856          0.5113      -0.0012513      -0.0013683
v  TurbEner             0.0010308        0.015114       0.0032885       0.0033475
v  Dissip              9.2048e-05        0.029472      0.00045114      0.00039009
v  TurbVisc               0.16791          11.333          4.7162          5.2773
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              710:        0.88865E-01

===============================================================


 INSTANT    0.711000000E+03   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000317E+04
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 :  0.23754E+00 0.12490E+01
   Friction velocity        uet   :  0.14211E-01 0.72753E-01
   Friction velocity        uk    :  0.17585E-01 0.38803E-01
   Dimensionless distance   yplus :  0.43156E+03 0.95354E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67048E+01      53   0.15905E-02   0.22000E-01 
c  VelocityX    0.46305E+04      13   0.63957E-02   0.43747E-03 
c  VelocityY    0.46305E+04      13   0.63957E-02   0.35991E-04 
c  VelocityZ    0.46305E+04      13   0.63957E-02   0.46549E-04 
c  TurbEner     0.59816E+01      13   0.11861E-03   0.15437E-08 
c  Dissip       0.14544E+01      16   0.20559E-02   0.50506E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.15           54511           26779           27273
v  Velocity[x]            0.29304          2.0203         0.90807         0.90984
v  Velocity[y]           -0.36761         0.70044      0.00055753      0.00033522
v  Velocity[z]           -0.42048         0.50455      -0.0012529      -0.0013708
v  TurbEner             0.0010315        0.015698       0.0032886       0.0033476
v  Dissip              9.2049e-05        0.031108      0.00045147      0.00039032
v  TurbVisc               0.16856          11.327          4.7164          5.2774
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              711:        0.89329E-01

===============================================================


 INSTANT    0.712000000E+03   TIME STEP NUMBER             712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000960E+04
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 :  0.23759E+00 0.13243E+01
   Friction velocity        uet   :  0.14213E-01 0.78931E-01
   Friction velocity        uk    :  0.17591E-01 0.38835E-01
   Dimensionless distance   yplus :  0.43205E+03 0.95356E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61391E+01      53   0.12746E-02   0.20132E-01 
c  VelocityX    0.46304E+04      13   0.71060E-02   0.34482E-03 
c  VelocityY    0.46304E+04      13   0.71060E-02   0.26842E-04 
c  VelocityZ    0.46304E+04      13   0.71060E-02   0.48765E-04 
c  TurbEner     0.59796E+01      13   0.13639E-03   0.21710E-08 
c  Dissip       0.14253E+01      16   0.19541E-02   0.55919E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.23           54514           26779           27273
v  Velocity[x]            0.29277          2.0891         0.90808         0.90985
v  Velocity[y]           -0.38233         0.69531      0.00054371      0.00032493
v  Velocity[z]           -0.42185           0.512      -0.0012542      -0.0013731
v  TurbEner              0.001036        0.015055       0.0032885       0.0033475
v  Dissip              9.2052e-05        0.029787      0.00045134      0.00039021
v  TurbVisc               0.16886           11.36          4.7163          5.2774
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              712:        0.89434E-01

===============================================================


 INSTANT    0.713000000E+03   TIME STEP NUMBER             713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999158E+04
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 :  0.23786E+00 0.12165E+01
   Friction velocity        uet   :  0.14229E-01 0.72328E-01
   Friction velocity        uk    :  0.17630E-01 0.38843E-01
   Dimensionless distance   yplus :  0.43212E+03 0.95346E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66468E+01      57   0.14553E-02   0.21786E-01 
c  VelocityX    0.46304E+04      12   0.72797E-02   0.33861E-03 
c  VelocityY    0.46304E+04      12   0.72797E-02   0.38103E-04 
c  VelocityZ    0.46304E+04      12   0.72797E-02   0.90149E-04 
c  TurbEner     0.59805E+01      13   0.67390E-04   0.81363E-09 
c  Dissip       0.14388E+01      13   0.32645E-03   0.25399E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -178.2           54528           26778           27272
v  Velocity[x]            0.29308          2.1516         0.90805         0.90983
v  Velocity[y]           -0.36612         0.70443      0.00055847      0.00033508
v  Velocity[z]           -0.42098         0.50662       -0.001238      -0.0013584
v  TurbEner             0.0010415        0.014955       0.0032886       0.0033475
v  Dissip              9.2094e-05        0.029676      0.00045141      0.00039025
v  TurbVisc               0.16902           11.34          4.7163          5.2774
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              713:        0.89532E-01

===============================================================


 INSTANT    0.714000000E+03   TIME STEP NUMBER             714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001840E+04
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 :  0.23779E+00 0.13249E+01
   Friction velocity        uet   :  0.14224E-01 0.78973E-01
   Friction velocity        uk    :  0.17676E-01 0.38829E-01
   Dimensionless distance   yplus :  0.43377E+03 0.95401E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64774E+01      57   0.16122E-02   0.21255E-01 
c  VelocityX    0.46303E+04      13   0.66516E-02   0.43065E-03 
c  VelocityY    0.46303E+04      13   0.66516E-02   0.22766E-04 
c  VelocityZ    0.46303E+04      13   0.66516E-02   0.59345E-04 
c  TurbEner     0.59803E+01      13   0.10975E-03   0.14176E-08 
c  Dissip       0.14458E+01      16   0.17127E-02   0.35913E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.46           54516           26779           27273
v  Velocity[x]            0.29255          1.9904         0.90807         0.90985
v  Velocity[y]           -0.38244         0.69165      0.00055859      0.00033708
v  Velocity[z]           -0.42089         0.51106      -0.0012419      -0.0013626
v  TurbEner             0.0010401        0.015479       0.0032886       0.0033476
v  Dissip              9.2096e-05        0.030978      0.00045161       0.0003904
v  TurbVisc               0.16998          11.338          4.7164          5.2775
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              714:        0.90122E-01

===============================================================


 INSTANT    0.715000000E+03   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998091E+04
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 :  0.23781E+00 0.12266E+01
   Friction velocity        uet   :  0.14226E-01 0.72590E-01
   Friction velocity        uk    :  0.17664E-01 0.38740E-01
   Dimensionless distance   yplus :  0.43384E+03 0.95400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57513E+01      54   0.11507E-02   0.18868E-01 
c  VelocityX    0.46303E+04      13   0.64818E-02   0.38463E-03 
c  VelocityY    0.46303E+04      13   0.64818E-02   0.24630E-04 
c  VelocityZ    0.46303E+04      13   0.64818E-02   0.36224E-04 
c  TurbEner     0.59784E+01      14   0.15643E-03   0.25507E-08 
c  Dissip       0.14088E+01      17   0.24571E-02   0.76670E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.33           54511           26778           27273
v  Velocity[x]             0.2927          2.0841         0.90804         0.90982
v  Velocity[y]           -0.36804         0.70132      0.00055276      0.00033106
v  Velocity[z]           -0.42267         0.50406      -0.0012568      -0.0013733
v  TurbEner             0.0010448        0.014695       0.0032884       0.0033474
v  Dissip              9.2098e-05        0.029264      0.00045135      0.00039021
v  TurbVisc               0.16988          11.375          4.7163          5.2774
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              715:        0.89996E-01

===============================================================


 INSTANT    0.716000000E+03   TIME STEP NUMBER             716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001938E+04
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 :  0.23761E+00 0.13238E+01
   Friction velocity        uet   :  0.14214E-01 0.78902E-01
   Friction velocity        uk    :  0.17704E-01 0.38655E-01
   Dimensionless distance   yplus :  0.43404E+03 0.95457E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60119E+01      55   0.13968E-02   0.19704E-01 
c  VelocityX    0.46303E+04      12   0.73538E-02   0.35923E-03 
c  VelocityY    0.46303E+04      12   0.73538E-02   0.22931E-04 
c  VelocityZ    0.46303E+04      12   0.73538E-02   0.42425E-04 
c  TurbEner     0.59783E+01      13   0.61667E-04   0.73621E-09 
c  Dissip       0.14075E+01      14   0.51530E-03   0.36058E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.89           54521           26778           27272
v  Velocity[x]            0.29299           2.128         0.90805         0.90984
v  Velocity[y]           -0.38266         0.69529      0.00054927       0.0003306
v  Velocity[z]           -0.41888         0.51168      -0.0012499      -0.0013703
v  TurbEner             0.0010463        0.014576       0.0032882       0.0033473
v  Dissip              9.2078e-05        0.028934      0.00045123      0.00039011
v  TurbVisc               0.16997          11.357          4.7164          5.2775
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              716:        0.89211E-01

===============================================================


 INSTANT    0.717000000E+03   TIME STEP NUMBER             717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001478E+04
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 :  0.23749E+00 0.12173E+01
   Friction velocity        uet   :  0.14207E-01 0.72566E-01
   Friction velocity        uk    :  0.17717E-01 0.38757E-01
   Dimensionless distance   yplus :  0.43489E+03 0.95400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58159E+01      57   0.14512E-02   0.19089E-01 
c  VelocityX    0.46303E+04      12   0.64315E-02   0.28446E-03 
c  VelocityY    0.46303E+04      12   0.64315E-02   0.38202E-04 
c  VelocityZ    0.46303E+04      12   0.64315E-02   0.11835E-03 
c  TurbEner     0.59790E+01      13   0.73215E-04   0.95793E-09 
c  Dissip       0.14272E+01      15   0.71784E-03   0.10508E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.61           54515           26778           27273
v  Velocity[x]            0.29269          2.1634         0.90805         0.90982
v  Velocity[y]           -0.36664         0.70193      0.00055938      0.00033571
v  Velocity[z]            -0.4204         0.50598      -0.0012365       -0.001358
v  TurbEner             0.0010439        0.014769       0.0032882       0.0033473
v  Dissip              9.2096e-05         0.02931      0.00045134      0.00039018
v  TurbVisc               0.17035          11.358          4.7163          5.2774
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              717:        0.89742E-01

===============================================================


 INSTANT    0.718000000E+03   TIME STEP NUMBER             718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997625E+04
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 :  0.23764E+00 0.13269E+01
   Friction velocity        uet   :  0.14217E-01 0.79094E-01
   Friction velocity        uk    :  0.17697E-01 0.38824E-01
   Dimensionless distance   yplus :  0.43488E+03 0.95350E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.52618E+01      57   0.11427E-02   0.17247E-01 
c  VelocityX    0.46302E+04      12   0.72602E-02   0.27915E-03 
c  VelocityY    0.46302E+04      12   0.72602E-02   0.27202E-04 
c  VelocityZ    0.46302E+04      12   0.72602E-02   0.49342E-04 
c  TurbEner     0.59794E+01      13   0.77415E-04   0.10979E-08 
c  Dissip       0.14569E+01      16   0.10827E-02   0.22315E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.44           54518           26779           27273
v  Velocity[x]            0.29269          2.1913         0.90805         0.90982
v  Velocity[y]            -0.3824         0.69555      0.00054877      0.00032775
v  Velocity[z]           -0.42013         0.51107      -0.0012462      -0.0013695
v  TurbEner             0.0010447        0.015008       0.0032881       0.0033471
v  Dissip              9.2042e-05        0.029944      0.00045149      0.00039028
v  TurbVisc               0.17012          11.332          4.7163          5.2774
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              718:        0.89697E-01

===============================================================


 INSTANT    0.719000000E+03   TIME STEP NUMBER             719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998135E+04
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 :  0.23814E+00 0.12215E+01
   Friction velocity        uet   :  0.14247E-01 0.72384E-01
   Friction velocity        uk    :  0.17703E-01 0.38825E-01
   Dimensionless distance   yplus :  0.43425E+03 0.95281E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65068E+01      54   0.16048E-02   0.21333E-01 
c  VelocityX    0.46302E+04      13   0.69371E-02   0.41592E-03 
c  VelocityY    0.46302E+04      13   0.69371E-02   0.21146E-04 
c  VelocityZ    0.46302E+04      13   0.69371E-02   0.27918E-04 
c  TurbEner     0.59800E+01      13   0.12018E-03   0.11651E-08 
c  Dissip       0.14793E+01      16   0.22430E-02   0.58078E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.53           54516           26779           27273
v  Velocity[x]            0.29289          2.0293         0.90805         0.90983
v  Velocity[y]           -0.36756         0.70422      0.00054645       0.0003223
v  Velocity[z]           -0.42108         0.50438       -0.001251      -0.0013689
v  TurbEner             0.0010458        0.015617       0.0032881       0.0033471
v  Dissip              9.2051e-05        0.031719      0.00045174      0.00039046
v  TurbVisc               0.16972          11.322          4.7163          5.2774
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              719:        0.89214E-01

===============================================================


 INSTANT    0.720000000E+03   TIME STEP NUMBER             720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000508E+04
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 :  0.23765E+00 0.13248E+01
   Friction velocity        uet   :  0.14219E-01 0.78968E-01
   Friction velocity        uk    :  0.17713E-01 0.38791E-01
   Dimensionless distance   yplus :  0.43512E+03 0.95229E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66646E+01      54   0.15321E-02   0.21866E-01 
c  VelocityX    0.46302E+04      13   0.68985E-02   0.37528E-03 
c  VelocityY    0.46302E+04      13   0.68985E-02   0.31426E-04 
c  VelocityZ    0.46302E+04      13   0.68985E-02   0.40776E-04 
c  TurbEner     0.59788E+01      13   0.13905E-03   0.20782E-08 
c  Dissip       0.14531E+01      16   0.18511E-02   0.51226E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.43           54497           26779           27273
v  Velocity[x]            0.29279          2.0917         0.90806         0.90984
v  Velocity[y]           -0.38229         0.69165      0.00053921      0.00032074
v  Velocity[z]           -0.42178         0.51186      -0.0012502       -0.001371
v  TurbEner             0.0010403        0.015006       0.0032879        0.003347
v  Dissip              9.2108e-05        0.030503      0.00045159      0.00039036
v  TurbVisc               0.17013          11.351          4.7162          5.2773
v  total_pressure           83078      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              720:        0.90090E-01

===============================================================


 INSTANT    0.721000000E+03   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999667E+04
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 :  0.23762E+00 0.12391E+01
   Friction velocity        uet   :  0.14218E-01 0.72587E-01
   Friction velocity        uk    :  0.17666E-01 0.38685E-01
   Dimensionless distance   yplus :  0.43439E+03 0.95201E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57164E+01      56   0.12937E-02   0.18748E-01 
c  VelocityX    0.46302E+04      12   0.65369E-02   0.33849E-03 
c  VelocityY    0.46302E+04      12   0.65369E-02   0.36204E-04 
c  VelocityZ    0.46302E+04      12   0.65369E-02   0.57551E-04 
c  TurbEner     0.59785E+01      12   0.68960E-04   0.87707E-09 
c  Dissip       0.14636E+01      13   0.21389E-03   0.15993E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.5           54513           26778           27273
v  Velocity[x]            0.29284          2.1448         0.90805         0.90982
v  Velocity[y]           -0.36617         0.70117      0.00055202       0.0003283
v  Velocity[z]           -0.42148         0.50646      -0.0012494      -0.0013697
v  TurbEner             0.0010416        0.014951       0.0032878       0.0033469
v  Dissip              9.2143e-05        0.030477      0.00045161      0.00039036
v  TurbVisc               0.16956          11.397          4.7162          5.2773
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              721:        0.89424E-01

===============================================================


 INSTANT    0.722000000E+03   TIME STEP NUMBER             722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001084E+04
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 :  0.23783E+00 0.13241E+01
   Friction velocity        uet   :  0.14231E-01 0.78925E-01
   Friction velocity        uk    :  0.17677E-01 0.38722E-01
   Dimensionless distance   yplus :  0.43386E+03 0.95173E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61334E+01      53   0.14285E-02   0.20106E-01 
c  VelocityX    0.46301E+04      12   0.74235E-02   0.31223E-03 
c  VelocityY    0.46301E+04      12   0.74235E-02   0.29951E-04 
c  VelocityZ    0.46301E+04      12   0.74235E-02   0.49438E-04 
c  TurbEner     0.59792E+01      13   0.68388E-04   0.82565E-09 
c  Dissip       0.14827E+01      15   0.86835E-03   0.19169E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.36           54518           26779           27273
v  Velocity[x]             0.2927          2.1772         0.90806         0.90983
v  Velocity[y]           -0.38243         0.69494       0.0005382      0.00031708
v  Velocity[z]           -0.42029           0.511      -0.0012506      -0.0013734
v  TurbEner             0.0010411        0.015011       0.0032878       0.0033469
v  Dissip              9.2161e-05        0.030647       0.0004518      0.00039049
v  TurbVisc               0.16928          11.382          4.7161          5.2772
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              722:        0.89142E-01

===============================================================


 INSTANT    0.723000000E+03   TIME STEP NUMBER             723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998134E+04
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 :  0.23733E+00 0.12459E+01
   Friction velocity        uet   :  0.14202E-01 0.72696E-01
   Friction velocity        uk    :  0.17673E-01 0.38788E-01
   Dimensionless distance   yplus :  0.43420E+03 0.95185E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71992E+01      58   0.15419E-02   0.23612E-01 
c  VelocityX    0.46302E+04      12   0.71370E-02   0.40504E-03 
c  VelocityY    0.46302E+04      12   0.71370E-02   0.32067E-04 
c  VelocityZ    0.46302E+04      12   0.71370E-02   0.94070E-04 
c  TurbEner     0.59802E+01      13   0.75702E-04   0.10040E-08 
c  Dissip       0.15158E+01      15   0.97737E-03   0.17214E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.81           54534           26778           27273
v  Velocity[x]            0.29257          2.2142         0.90806         0.90984
v  Velocity[y]           -0.36803         0.70304      0.00055816      0.00033495
v  Velocity[z]           -0.41981         0.50396      -0.0012364       -0.001357
v  TurbEner             0.0010376        0.015225       0.0032878       0.0033468
v  Dissip              9.2185e-05         0.03128      0.00045208      0.00039069
v  TurbVisc               0.16946          11.332          4.7162          5.2773
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              723:        0.89696E-01

===============================================================


 INSTANT    0.724000000E+03   TIME STEP NUMBER             724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001221E+04
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 :  0.23791E+00 0.13243E+01
   Friction velocity        uet   :  0.14237E-01 0.78940E-01
   Friction velocity        uk    :  0.17643E-01 0.38793E-01
   Dimensionless distance   yplus :  0.43384E+03 0.95192E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67511E+01      56   0.14903E-02   0.22137E-01 
c  VelocityX    0.46300E+04      12   0.71129E-02   0.43686E-03 
c  VelocityY    0.46300E+04      12   0.71129E-02   0.26077E-04 
c  VelocityZ    0.46300E+04      12   0.71129E-02   0.51106E-04 
c  TurbEner     0.59801E+01      13   0.13943E-03   0.17005E-08 
c  Dissip       0.15336E+01      16   0.23904E-02   0.65512E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.6           54515           26779           27273
v  Velocity[x]            0.29285          2.0306         0.90806         0.90984
v  Velocity[y]           -0.38301         0.69575       0.0005472      0.00032515
v  Velocity[z]           -0.42158          0.5113      -0.0012507      -0.0013725
v  TurbEner             0.0010377        0.015929       0.0032878       0.0033468
v  Dissip              9.2201e-05        0.033202      0.00045236      0.00039089
v  TurbVisc               0.16913          11.321          4.7161          5.2772
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              724:        0.89312E-01

===============================================================


 INSTANT    0.725000000E+03   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999092E+04
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 :  0.23795E+00 0.12470E+01
   Friction velocity        uet   :  0.14240E-01 0.72722E-01
   Friction velocity        uk    :  0.17644E-01 0.38695E-01
   Dimensionless distance   yplus :  0.43296E+03 0.95167E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66654E+01      55   0.14587E-02   0.21838E-01 
c  VelocityX    0.46301E+04      12   0.70425E-02   0.43934E-03 
c  VelocityY    0.46301E+04      12   0.70425E-02   0.35503E-04 
c  VelocityZ    0.46301E+04      12   0.70425E-02   0.34611E-04 
c  TurbEner     0.59791E+01      13   0.14501E-03   0.20394E-08 
c  Dissip       0.15090E+01      16   0.20189E-02   0.57283E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.93           54523           26778           27272
v  Velocity[x]            0.29312          2.1166         0.90806         0.90984
v  Velocity[y]            -0.3681         0.70194      0.00055438      0.00033186
v  Velocity[z]            -0.4216         0.50698      -0.0012531      -0.0013729
v  TurbEner              0.001039        0.015245       0.0032876       0.0033467
v  Dissip              9.2146e-05        0.031792      0.00045224       0.0003908
v  TurbVisc               0.16865          11.356           4.716          5.2771
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              725:        0.90004E-01

===============================================================


 INSTANT    0.726000000E+03   TIME STEP NUMBER             726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001617E+04
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 :  0.23750E+00 0.13262E+01
   Friction velocity        uet   :  0.14213E-01 0.79050E-01
   Friction velocity        uk    :  0.17655E-01 0.38713E-01
   Dimensionless distance   yplus :  0.43373E+03 0.95169E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70532E+01      60   0.16252E-02   0.23139E-01 
c  VelocityX    0.46301E+04      13   0.67718E-02   0.39243E-03 
c  VelocityY    0.46301E+04      13   0.67718E-02   0.44801E-04 
c  VelocityZ    0.46301E+04      13   0.67718E-02   0.48764E-04 
c  TurbEner     0.59789E+01      12   0.68226E-04   0.10392E-08 
c  Dissip       0.15166E+01      14   0.34770E-03   0.34702E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.54           54515           26779           27273
v  Velocity[x]            0.29273          2.1497         0.90807         0.90985
v  Velocity[y]           -0.38277         0.69492      0.00054871      0.00032909
v  Velocity[z]           -0.42142         0.51386      -0.0012425      -0.0013635
v  TurbEner             0.0010339        0.015186       0.0032875       0.0033466
v  Dissip              9.2116e-05        0.031697       0.0004523      0.00039085
v  TurbVisc               0.16902          11.338          4.7159           5.277
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              726:        0.91041E-01

===============================================================


 INSTANT    0.727000000E+03   TIME STEP NUMBER             727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998515E+04
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 :  0.23782E+00 0.12144E+01
   Friction velocity        uet   :  0.14233E-01 0.72355E-01
   Friction velocity        uk    :  0.17612E-01 0.38674E-01
   Dimensionless distance   yplus :  0.43300E+03 0.95171E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69046E+01      58   0.14009E-02   0.22637E-01 
c  VelocityX    0.46300E+04      12   0.68720E-02   0.32886E-03 
c  VelocityY    0.46300E+04      12   0.68720E-02   0.42424E-04 
c  VelocityZ    0.46300E+04      12   0.68720E-02   0.12290E-03 
c  TurbEner     0.59788E+01      13   0.10687E-03   0.14696E-08 
c  Dissip       0.15284E+01      15   0.16514E-02   0.33720E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.54           54521           26777           27272
v  Velocity[x]            0.29276          2.0112         0.90804         0.90981
v  Velocity[y]           -0.36651         0.70281      0.00056217      0.00033847
v  Velocity[z]           -0.42158          0.5079      -0.0012405      -0.0013626
v  TurbEner             0.0010353        0.015652       0.0032874       0.0033464
v  Dissip              9.2065e-05        0.032975      0.00045246      0.00039095
v  TurbVisc               0.16842          11.338          4.7157          5.2768
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              727:        0.90374E-01

===============================================================


 INSTANT    0.728000000E+03   TIME STEP NUMBER             728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001675E+04
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 :  0.23773E+00 0.13248E+01
   Friction velocity        uet   :  0.14228E-01 0.78972E-01
   Friction velocity        uk    :  0.17624E-01 0.38737E-01
   Dimensionless distance   yplus :  0.43247E+03 0.95162E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62181E+01      55   0.14346E-02   0.20389E-01 
c  VelocityX    0.46300E+04      12   0.70196E-02   0.36237E-03 
c  VelocityY    0.46300E+04      12   0.70196E-02   0.29220E-04 
c  VelocityZ    0.46300E+04      12   0.70196E-02   0.50514E-04 
c  TurbEner     0.59774E+01      13   0.14255E-03   0.18926E-08 
c  Dissip       0.14905E+01      16   0.23631E-02   0.73722E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.81           54515           26778           27272
v  Velocity[x]            0.29274          2.0866         0.90807         0.90984
v  Velocity[y]            -0.3827         0.69249      0.00054961       0.0003299
v  Velocity[z]           -0.41915         0.51205      -0.0012465      -0.0013694
v  TurbEner             0.0010346        0.014972       0.0032871       0.0033462
v  Dissip              9.2101e-05         0.03133      0.00045218      0.00039075
v  TurbVisc               0.16808          11.364          4.7155          5.2766
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              728:        0.89697E-01

===============================================================


 INSTANT    0.729000000E+03   TIME STEP NUMBER             729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000354E+04
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 :  0.23746E+00 0.12369E+01
   Friction velocity        uet   :  0.14213E-01 0.72564E-01
   Friction velocity        uk    :  0.17618E-01 0.38769E-01
   Dimensionless distance   yplus :  0.43281E+03 0.95134E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62134E+01      56   0.13786E-02   0.20371E-01 
c  VelocityX    0.46301E+04      12   0.64367E-02   0.36269E-03 
c  VelocityY    0.46301E+04      12   0.64367E-02   0.24819E-04 
c  VelocityZ    0.46301E+04      12   0.64367E-02   0.30270E-04 
c  TurbEner     0.59772E+01      12   0.72415E-04   0.90428E-09 
c  Dissip       0.14890E+01      14   0.57157E-03   0.44045E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.17           54502           26777           27272
v  Velocity[x]            0.29276          2.1473         0.90806         0.90983
v  Velocity[y]           -0.36824         0.70063       0.0005502      0.00032792
v  Velocity[z]           -0.42105         0.50493      -0.0012379      -0.0013569
v  TurbEner               0.00103        0.014798       0.0032869        0.003346
v  Dissip              9.2052e-05        0.030956      0.00045212      0.00039071
v  TurbVisc               0.16816          11.342          4.7154          5.2765
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              729:        0.89159E-01

===============================================================


 INSTANT    0.730000000E+03   TIME STEP NUMBER             730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001499E+04
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 :  0.23768E+00 0.13243E+01
   Friction velocity        uet   :  0.14226E-01 0.78942E-01
   Friction velocity        uk    :  0.17579E-01 0.38751E-01
   Dimensionless distance   yplus :  0.43233E+03 0.95116E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60452E+01      54   0.12141E-02   0.19822E-01 
c  VelocityX    0.46300E+04      12   0.69654E-02   0.30744E-03 
c  VelocityY    0.46300E+04      12   0.69654E-02   0.25903E-04 
c  VelocityZ    0.46300E+04      12   0.69654E-02   0.48316E-04 
c  TurbEner     0.59774E+01      12   0.65178E-04   0.83191E-09 
c  Dissip       0.15069E+01      14   0.57110E-03   0.77371E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.01           54506           26777           27272
v  Velocity[x]            0.29281          2.1738         0.90806         0.90983
v  Velocity[y]           -0.38258         0.69346      0.00054334      0.00032397
v  Velocity[z]           -0.42226         0.51229      -0.0012489       -0.001372
v  TurbEner             0.0010289        0.014887       0.0032867       0.0033459
v  Dissip              9.2044e-05        0.031176      0.00045217      0.00039074
v  TurbVisc               0.16769          11.352          4.7151          5.2762
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              730:        0.88990E-01

===============================================================


 INSTANT    0.731000000E+03   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000359E+04
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 :  0.23773E+00 0.12169E+01
   Friction velocity        uet   :  0.14229E-01 0.72546E-01
   Friction velocity        uk    :  0.17569E-01 0.38711E-01
   Dimensionless distance   yplus :  0.43126E+03 0.95136E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71225E+01      55   0.15222E-02   0.23340E-01 
c  VelocityX    0.46300E+04      12   0.72054E-02   0.39640E-03 
c  VelocityY    0.46300E+04      12   0.72054E-02   0.24714E-04 
c  VelocityZ    0.46300E+04      12   0.72054E-02   0.12155E-03 
c  TurbEner     0.59776E+01      13   0.11730E-03   0.11681E-08 
c  Dissip       0.15175E+01      15   0.18572E-02   0.36465E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.42           54513           26776           27270
v  Velocity[x]            0.29304          2.0174         0.90804         0.90982
v  Velocity[y]           -0.36623         0.70132      0.00055708      0.00033458
v  Velocity[z]           -0.42121         0.50678      -0.0012474      -0.0013704
v  TurbEner             0.0010288        0.015461       0.0032866       0.0033457
v  Dissip              9.2005e-05        0.032645      0.00045226      0.00039081
v  TurbVisc               0.16707          11.331           4.715          5.2761
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              731:        0.89932E-01

===============================================================


 INSTANT    0.732000000E+03   TIME STEP NUMBER             732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002177E+04
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 :  0.23782E+00 0.13241E+01
   Friction velocity        uet   :  0.14234E-01 0.78926E-01
   Friction velocity        uk    :  0.17568E-01 0.38738E-01
   Dimensionless distance   yplus :  0.43180E+03 0.95178E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67361E+01      64   0.15965E-02   0.22108E-01 
c  VelocityX    0.46299E+04      12   0.63823E-02   0.36527E-03 
c  VelocityY    0.46299E+04      12   0.63823E-02   0.44147E-04 
c  VelocityZ    0.46299E+04      12   0.63823E-02   0.50242E-04 
c  TurbEner     0.59758E+01      13   0.13868E-03   0.19319E-08 
c  Dissip       0.14779E+01      16   0.23805E-02   0.76195E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.53           54501           26777           27271
v  Velocity[x]            0.29221          2.0866         0.90807         0.90985
v  Velocity[y]           -0.38249           0.694      0.00055059      0.00033179
v  Velocity[z]           -0.42111         0.51115      -0.0012372      -0.0013562
v  TurbEner             0.0010225        0.014824       0.0032862       0.0033455
v  Dissip              9.2028e-05        0.031043      0.00045194      0.00039059
v  TurbVisc               0.16732          11.328          4.7148          5.2759
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              732:        0.92242E-01

===============================================================


 INSTANT    0.733000000E+03   TIME STEP NUMBER             733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999384E+04
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 :  0.23773E+00 0.12340E+01
   Friction velocity        uet   :  0.14229E-01 0.72519E-01
   Friction velocity        uk    :  0.17514E-01 0.38699E-01
   Dimensionless distance   yplus :  0.43084E+03 0.95249E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67805E+01      60   0.13091E-02   0.22221E-01 
c  VelocityX    0.46300E+04      12   0.72117E-02   0.34385E-03 
c  VelocityY    0.46300E+04      12   0.72117E-02   0.45857E-04 
c  VelocityZ    0.46300E+04      12   0.72117E-02   0.29983E-04 
c  TurbEner     0.59755E+01      12   0.67000E-04   0.89741E-09 
c  Dissip       0.14781E+01      14   0.57729E-03   0.41572E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.55           54507           26777           27271
v  Velocity[x]            0.29267          2.1523         0.90804         0.90981
v  Velocity[y]           -0.36814          0.7005      0.00055334      0.00033089
v  Velocity[z]           -0.42279         0.50407      -0.0012458      -0.0013635
v  TurbEner             0.0010232        0.014673       0.0032859       0.0033453
v  Dissip               9.204e-05        0.030647      0.00045181      0.00039049
v  TurbVisc               0.16665           11.36          4.7146          5.2757
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              733:        0.89975E-01

===============================================================


 INSTANT    0.734000000E+03   TIME STEP NUMBER             734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000442E+04
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 :  0.23745E+00 0.13256E+01
   Friction velocity        uet   :  0.14212E-01 0.79010E-01
   Friction velocity        uk    :  0.17521E-01 0.38732E-01
   Dimensionless distance   yplus :  0.43016E+03 0.95223E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69238E+01      57   0.13574E-02   0.22691E-01 
c  VelocityX    0.46300E+04      12   0.69455E-02   0.35981E-03 
c  VelocityY    0.46300E+04      12   0.69455E-02   0.36239E-04 
c  VelocityZ    0.46300E+04      12   0.69455E-02   0.40943E-04 
c  TurbEner     0.59760E+01      13   0.77482E-04   0.90397E-09 
c  Dissip       0.14944E+01      15   0.68191E-03   0.10402E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.28           54521           26777           27271
v  Velocity[x]            0.29333           2.175         0.90806         0.90983
v  Velocity[y]           -0.38294         0.69383      0.00053669      0.00031766
v  Velocity[z]           -0.41888         0.51143      -0.0012408      -0.0013591
v  TurbEner             0.0010227        0.014829       0.0032857       0.0033451
v  Dissip              9.1982e-05        0.030931      0.00045183      0.00039049
v  TurbVisc               0.16637           11.34          4.7144          5.2755
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              734:        0.90496E-01

===============================================================


 INSTANT    0.735000000E+03   TIME STEP NUMBER             735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999937E+04
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 :  0.23755E+00 0.12532E+01
   Friction velocity        uet   :  0.14219E-01 0.73025E-01
   Friction velocity        uk    :  0.17516E-01 0.38754E-01
   Dimensionless distance   yplus :  0.43045E+03 0.95229E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62317E+01      52   0.13503E-02   0.20434E-01 
c  VelocityX    0.46299E+04      12   0.63675E-02   0.38458E-03 
c  VelocityY    0.46299E+04      12   0.63675E-02   0.30948E-04 
c  VelocityZ    0.46299E+04      12   0.63675E-02   0.43847E-04 
c  TurbEner     0.59764E+01      12   0.12146E-03   0.11928E-08 
c  Dissip       0.15099E+01      16   0.19490E-02   0.41085E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.84           54533           26776           27270
v  Velocity[x]            0.29266          2.0222         0.90805         0.90982
v  Velocity[y]           -0.36799         0.70197      0.00054212       0.0003193
v  Velocity[z]           -0.42054         0.50707      -0.0012554      -0.0013743
v  TurbEner             0.0010193         0.01542       0.0032856       0.0033449
v  Dissip              9.1977e-05        0.032457      0.00045195      0.00039058
v  TurbVisc               0.16656          11.342          4.7142          5.2754
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              735:        0.90129E-01

===============================================================


 INSTANT    0.736000000E+03   TIME STEP NUMBER             736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001809E+04
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 :  0.23766E+00 0.13245E+01
   Friction velocity        uet   :  0.14225E-01 0.78952E-01
   Friction velocity        uk    :  0.17487E-01 0.38756E-01
   Dimensionless distance   yplus :  0.43011E+03 0.95217E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63067E+01      55   0.13309E-02   0.20684E-01 
c  VelocityX    0.46299E+04      12   0.68482E-02   0.35349E-03 
c  VelocityY    0.46299E+04      12   0.68482E-02   0.27823E-04 
c  VelocityZ    0.46299E+04      12   0.68482E-02   0.45715E-04 
c  TurbEner     0.59748E+01      13   0.13606E-03   0.17396E-08 
c  Dissip       0.14715E+01      16   0.23725E-02   0.74001E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.58           54546           26777           27271
v  Velocity[x]            0.29258          2.0942         0.90807         0.90984
v  Velocity[y]           -0.38286         0.69315      0.00053541      0.00031772
v  Velocity[z]           -0.42048         0.51374      -0.0012493      -0.0013703
v  TurbEner             0.0010197        0.014789       0.0032852       0.0033447
v  Dissip              9.1974e-05        0.030849      0.00045161      0.00039034
v  TurbVisc               0.16629          11.315           4.714          5.2752
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              736:        0.90965E-01

===============================================================


 INSTANT    0.737000000E+03   TIME STEP NUMBER             737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998790E+04
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 :  0.23803E+00 0.12385E+01
   Friction velocity        uet   :  0.14247E-01 0.72457E-01
   Friction velocity        uk    :  0.17491E-01 0.38771E-01
   Dimensionless distance   yplus :  0.42930E+03 0.95133E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66820E+01      58   0.13264E-02   0.21892E-01 
c  VelocityX    0.46299E+04      12   0.70124E-02   0.29262E-03 
c  VelocityY    0.46299E+04      12   0.70124E-02   0.31434E-04 
c  VelocityZ    0.46299E+04      12   0.70124E-02   0.86512E-04 
c  TurbEner     0.59755E+01      13   0.65565E-04   0.74065E-09 
c  Dissip       0.14778E+01      13   0.43095E-03   0.26063E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.36           54549           26776           27270
v  Velocity[x]             0.2929          2.1567         0.90806         0.90983
v  Velocity[y]           -0.36665         0.69983       0.0005481      0.00032628
v  Velocity[z]           -0.42118         0.50788      -0.0012394      -0.0013601
v  TurbEner             0.0010216        0.014718       0.0032851       0.0033446
v  Dissip              9.1999e-05        0.030578      0.00045153      0.00039027
v  TurbVisc                0.1659          11.313          4.7138           5.275
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              737:        0.90474E-01

===============================================================


 INSTANT    0.738000000E+03   TIME STEP NUMBER             738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001549E+04
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 :  0.23770E+00 0.13250E+01
   Friction velocity        uet   :  0.14228E-01 0.78986E-01
   Friction velocity        uk    :  0.17507E-01 0.38791E-01
   Dimensionless distance   yplus :  0.43016E+03 0.95133E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68074E+01      57   0.14818E-02   0.22321E-01 
c  VelocityX    0.46299E+04      12   0.75734E-02   0.42816E-03 
c  VelocityY    0.46299E+04      12   0.75734E-02   0.25070E-04 
c  VelocityZ    0.46299E+04      12   0.75734E-02   0.58894E-04 
c  TurbEner     0.59755E+01      13   0.11827E-03   0.14571E-08 
c  Dissip       0.14806E+01      16   0.16948E-02   0.32715E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.18           54541           26776           27270
v  Velocity[x]            0.29276          1.9944         0.90807         0.90985
v  Velocity[y]           -0.38272         0.69148      0.00054899      0.00032872
v  Velocity[z]           -0.42194         0.51207      -0.0012547      -0.0013762
v  TurbEner             0.0010174        0.015279       0.0032852       0.0033446
v  Dissip              9.2002e-05        0.031854      0.00045162      0.00039035
v  TurbVisc               0.16636          11.351          4.7137          5.2749
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              738:        0.89989E-01

===============================================================


 INSTANT    0.739000000E+03   TIME STEP NUMBER             739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999057E+04
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 :  0.23755E+00 0.12352E+01
   Friction velocity        uet   :  0.14219E-01 0.72457E-01
   Friction velocity        uk    :  0.17470E-01 0.38697E-01
   Dimensionless distance   yplus :  0.42956E+03 0.95156E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66868E+01      57   0.16255E-02   0.21924E-01 
c  VelocityX    0.46299E+04      12   0.69684E-02   0.46214E-03 
c  VelocityY    0.46299E+04      12   0.69684E-02   0.33558E-04 
c  VelocityZ    0.46299E+04      12   0.69684E-02   0.32835E-04 
c  TurbEner     0.59743E+01      14   0.15624E-03   0.26064E-08 
c  Dissip       0.14399E+01      17   0.27712E-02   0.90860E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.96           54518           26776           27271
v  Velocity[x]            0.29287          2.0905         0.90807         0.90984
v  Velocity[y]           -0.36821         0.69984      0.00055678      0.00033474
v  Velocity[z]           -0.42164          0.5048      -0.0012398      -0.0013553
v  TurbEner             0.0010198         0.01452       0.0032849       0.0033443
v  Dissip              9.2011e-05        0.029927      0.00045128      0.00039012
v  TurbVisc                0.1659          11.339          4.7136          5.2748
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              739:        0.89889E-01

===============================================================


 INSTANT    0.740000000E+03   TIME STEP NUMBER             740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998219E+04
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 :  0.23781E+00 0.13224E+01
   Friction velocity        uet   :  0.14235E-01 0.78828E-01
   Friction velocity        uk    :  0.17491E-01 0.38702E-01
   Dimensionless distance   yplus :  0.42918E+03 0.95152E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68500E+01      59   0.13959E-02   0.22452E-01 
c  VelocityX    0.46298E+04      12   0.67674E-02   0.36505E-03 
c  VelocityY    0.46298E+04      12   0.67674E-02   0.45058E-04 
c  VelocityZ    0.46298E+04      12   0.67674E-02   0.47887E-04 
c  TurbEner     0.59738E+01      13   0.65449E-04   0.11587E-08 
c  Dissip       0.14352E+01      14   0.59991E-03   0.52228E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.45           54526           26777           27271
v  Velocity[x]            0.29281           2.131         0.90804         0.90982
v  Velocity[y]           -0.38273         0.69327      0.00055356      0.00033435
v  Velocity[z]           -0.42039         0.51221      -0.0012448      -0.0013624
v  TurbEner             0.0010195        0.014468       0.0032848       0.0033443
v  Dissip              9.1979e-05        0.029543      0.00045112         0.00039
v  TurbVisc               0.16569          11.324          4.7134          5.2746
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              740:        0.89638E-01

===============================================================


 INSTANT    0.741000000E+03   TIME STEP NUMBER             741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998596E+04
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 :  0.23730E+00 0.12152E+01
   Friction velocity        uet   :  0.14204E-01 0.72452E-01
   Friction velocity        uk    :  0.17489E-01 0.38738E-01
   Dimensionless distance   yplus :  0.42955E+03 0.95178E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66085E+01      59   0.13433E-02   0.21668E-01 
c  VelocityX    0.46299E+04      12   0.72339E-02   0.34286E-03 
c  VelocityY    0.46299E+04      12   0.72339E-02   0.43991E-04 
c  VelocityZ    0.46299E+04      12   0.72339E-02   0.99264E-04 
c  TurbEner     0.59751E+01      13   0.80903E-04   0.11847E-08 
c  Dissip       0.14536E+01      15   0.63373E-03   0.93098E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.27           54528           26776           27271
v  Velocity[x]            0.29257          2.1759         0.90805         0.90982
v  Velocity[y]           -0.36676         0.70013      0.00056215      0.00033866
v  Velocity[z]            -0.4198         0.50632      -0.0012375       -0.001358
v  TurbEner             0.0010165        0.014645       0.0032848       0.0033443
v  Dissip              9.1978e-05        0.029771      0.00045117      0.00039004
v  TurbVisc               0.16584          11.356          4.7134          5.2745
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              741:        0.89870E-01

===============================================================


 INSTANT    0.742000000E+03   TIME STEP NUMBER             742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001331E+04
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 :  0.23799E+00 0.13250E+01
   Friction velocity        uet   :  0.14246E-01 0.78993E-01
   Friction velocity        uk    :  0.17463E-01 0.38772E-01
   Dimensionless distance   yplus :  0.42933E+03 0.95206E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65124E+01      59   0.16330E-02   0.21352E-01 
c  VelocityX    0.46298E+04      12   0.69782E-02   0.46365E-03 
c  VelocityY    0.46298E+04      12   0.69782E-02   0.45673E-04 
c  VelocityZ    0.46298E+04      12   0.69782E-02   0.50805E-04 
c  TurbEner     0.59755E+01      13   0.12347E-03   0.16324E-08 
c  Dissip       0.14615E+01      16   0.17929E-02   0.35910E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.93           54505           26777           27271
v  Velocity[x]             0.2927            2.01         0.90806         0.90984
v  Velocity[y]           -0.38243          0.6939      0.00055341      0.00033598
v  Velocity[z]           -0.42143         0.51132      -0.0012419      -0.0013604
v  TurbEner             0.0010169        0.015227        0.003285       0.0033444
v  Dissip              9.1982e-05        0.031137       0.0004513      0.00039014
v  TurbVisc               0.16557          11.335          4.7133          5.2744
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              742:        0.91140E-01

===============================================================


 INSTANT    0.743000000E+03   TIME STEP NUMBER             743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999144E+04
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 :  0.23771E+00 0.12490E+01
   Friction velocity        uet   :  0.14229E-01 0.72832E-01
   Friction velocity        uk    :  0.17466E-01 0.38778E-01
   Dimensionless distance   yplus :  0.42866E+03 0.95257E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59906E+01      55   0.12096E-02   0.19631E-01 
c  VelocityX    0.46299E+04      12   0.68603E-02   0.37316E-03 
c  VelocityY    0.46299E+04      12   0.68603E-02   0.32589E-04 
c  VelocityZ    0.46299E+04      12   0.68603E-02   0.29724E-04 
c  TurbEner     0.59740E+01      14   0.13417E-03   0.22969E-08 
c  Dissip       0.14315E+01      17   0.21199E-02   0.66231E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.92           54511           26776           27270
v  Velocity[x]            0.29299          2.1001         0.90805         0.90983
v  Velocity[y]           -0.36755         0.70256      0.00055075      0.00033027
v  Velocity[z]           -0.42129         0.50456      -0.0012401      -0.0013577
v  TurbEner             0.0010181        0.014633       0.0032847       0.0033442
v  Dissip              9.2009e-05        0.029794        0.000451      0.00038993
v  TurbVisc                0.1652          11.326          4.7133          5.2745
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              743:        0.90082E-01

===============================================================


 INSTANT    0.744000000E+03   TIME STEP NUMBER             744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001724E+04
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 :  0.23758E+00 0.13248E+01
   Friction velocity        uet   :  0.14220E-01 0.78975E-01
   Friction velocity        uk    :  0.17477E-01 0.38782E-01
   Dimensionless distance   yplus :  0.42949E+03 0.95283E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56168E+01      53   0.14517E-02   0.18426E-01 
c  VelocityX    0.46299E+04      12   0.71813E-02   0.30826E-03 
c  VelocityY    0.46299E+04      12   0.71813E-02   0.26043E-04 
c  VelocityZ    0.46299E+04      12   0.71813E-02   0.40254E-04 
c  TurbEner     0.59742E+01      13   0.61434E-04   0.69179E-09 
c  Dissip       0.14381E+01      14   0.33402E-03   0.24429E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.75           54519           26777           27271
v  Velocity[x]            0.29251          2.1417         0.90806         0.90984
v  Velocity[y]           -0.38231         0.69239      0.00054292      0.00032419
v  Velocity[z]           -0.42129         0.51197      -0.0012519      -0.0013709
v  TurbEner             0.0010127        0.014615       0.0032846       0.0033441
v  Dissip              9.2029e-05        0.029692      0.00045097      0.00038991
v  TurbVisc               0.16561          11.356          4.7131          5.2743
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              744:        0.89239E-01

===============================================================


 INSTANT    0.745000000E+03   TIME STEP NUMBER             745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999405E+04
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 :  0.23781E+00 0.12173E+01
   Friction velocity        uet   :  0.14233E-01 0.72565E-01
   Friction velocity        uk    :  0.17430E-01 0.38699E-01
   Dimensionless distance   yplus :  0.42869E+03 0.95323E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68646E+01      65   0.15404E-02   0.22503E-01 
c  VelocityX    0.46299E+04      12   0.74954E-02   0.37593E-03 
c  VelocityY    0.46299E+04      12   0.74954E-02   0.27769E-04 
c  VelocityZ    0.46299E+04      12   0.74954E-02   0.11358E-03 
c  TurbEner     0.59750E+01      13   0.76620E-04   0.91522E-09 
c  Dissip       0.14588E+01      15   0.80653E-03   0.13729E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.48           54523           26776           27271
v  Velocity[x]            0.29248          2.1734         0.90806         0.90984
v  Velocity[y]           -0.36614         0.70058      0.00056386      0.00034239
v  Velocity[z]           -0.42135         0.50664      -0.0012343      -0.0013522
v  TurbEner              0.001014        0.014827       0.0032845       0.0033441
v  Dissip              9.2084e-05        0.030071      0.00045106      0.00038997
v  TurbVisc               0.16499          11.344          4.7131          5.2743
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              745:        0.91333E-01

===============================================================


 INSTANT    0.746000000E+03   TIME STEP NUMBER             746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000009E+04
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 :  0.23773E+00 0.13243E+01
   Friction velocity        uet   :  0.14228E-01 0.78947E-01
   Friction velocity        uk    :  0.17442E-01 0.38614E-01
   Dimensionless distance   yplus :  0.42820E+03 0.95358E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67504E+01      67   0.13413E-02   0.22129E-01 
c  VelocityX    0.46299E+04      12   0.67528E-02   0.38797E-03 
c  VelocityY    0.46299E+04      12   0.67528E-02   0.49555E-04 
c  VelocityZ    0.46299E+04      12   0.67528E-02   0.56435E-04 
c  TurbEner     0.59757E+01      13   0.92001E-04   0.13823E-08 
c  Dissip       0.14824E+01      15   0.94368E-03   0.18634E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.97           54513           26777           27271
v  Velocity[x]            0.29325          2.1889         0.90804         0.90982
v  Velocity[y]           -0.38239         0.69349      0.00054675      0.00032617
v  Velocity[z]           -0.41913         0.51108      -0.0012467      -0.0013673
v  TurbEner             0.0010134        0.015069       0.0032847       0.0033442
v  Dissip              9.2132e-05        0.030582      0.00045125      0.00039009
v  TurbVisc               0.16485           11.35           4.713          5.2742
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              746:        0.91503E-01

===============================================================


 INSTANT    0.747000000E+03   TIME STEP NUMBER             747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999002E+04
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 :  0.23744E+00 0.12451E+01
   Friction velocity        uet   :  0.14209E-01 0.72674E-01
   Friction velocity        uk    :  0.17436E-01 0.38735E-01
   Dimensionless distance   yplus :  0.42851E+03 0.95319E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71248E+01      57   0.16850E-02   0.23361E-01 
c  VelocityX    0.46300E+04      13   0.68488E-02   0.35818E-03 
c  VelocityY    0.46300E+04      13   0.68488E-02   0.48628E-04 
c  VelocityZ    0.46300E+04      13   0.68488E-02   0.28525E-04 
c  TurbEner     0.59766E+01      13   0.12329E-03   0.13312E-08 
c  Dissip       0.15046E+01      16   0.21960E-02   0.55277E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.3           54515           26776           27270
v  Velocity[x]            0.29273          2.0373         0.90805         0.90982
v  Velocity[y]           -0.36796         0.70149      0.00054827      0.00032638
v  Velocity[z]           -0.42096           0.504       -0.001246      -0.0013641
v  TurbEner             0.0010104         0.01569       0.0032847       0.0033442
v  Dissip              9.2148e-05        0.032324      0.00045152      0.00039028
v  TurbVisc               0.16508          11.329           4.713          5.2742
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              747:        0.90663E-01

===============================================================


 INSTANT    0.748000000E+03   TIME STEP NUMBER             748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001524E+04
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 :  0.23778E+00 0.13240E+01
   Friction velocity        uet   :  0.14229E-01 0.78924E-01
   Friction velocity        uk    :  0.17411E-01 0.38817E-01
   Dimensionless distance   yplus :  0.42821E+03 0.95336E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68860E+01      58   0.15365E-02   0.22586E-01 
c  VelocityX    0.46298E+04      12   0.70528E-02   0.34668E-03 
c  VelocityY    0.46298E+04      12   0.70528E-02   0.34394E-04 
c  VelocityZ    0.46298E+04      12   0.70528E-02   0.43907E-04 
c  TurbEner     0.59756E+01      13   0.12273E-03   0.15968E-08 
c  Dissip       0.14806E+01      16   0.17181E-02   0.43114E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.36           54501           26777           27271
v  Velocity[x]            0.29245          2.0989         0.90806         0.90984
v  Velocity[y]           -0.38298         0.69399       0.0005485       0.0003311
v  Velocity[z]           -0.42229         0.51134      -0.0012433      -0.0013617
v  TurbEner             0.0010114        0.015149       0.0032847       0.0033442
v  Dissip              9.2096e-05        0.031158      0.00045139       0.0003902
v  TurbVisc               0.16491          11.324          4.7129          5.2741
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              748:        0.90275E-01

===============================================================


 INSTANT    0.749000000E+03   TIME STEP NUMBER             749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998585E+04
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 :  0.23768E+00 0.12490E+01
   Friction velocity        uet   :  0.14221E-01 0.72766E-01
   Friction velocity        uk    :  0.17419E-01 0.38817E-01
   Dimensionless distance   yplus :  0.42753E+03 0.95331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63810E+01      57   0.13281E-02   0.20910E-01 
c  VelocityX    0.46300E+04      13   0.74931E-02   0.41949E-03 
c  VelocityY    0.46300E+04      13   0.74931E-02   0.29982E-04 
c  VelocityZ    0.46300E+04      13   0.74931E-02   0.58850E-04 
c  TurbEner     0.59750E+01      13   0.70889E-04   0.10050E-08 
c  Dissip       0.14882E+01      13   0.19408E-03   0.15566E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.12           54507           26776           27270
v  Velocity[x]            0.29309          2.1497         0.90806         0.90983
v  Velocity[y]           -0.36797         0.70068      0.00055346      0.00033112
v  Velocity[z]           -0.42122           0.507      -0.0012501       -0.001366
v  TurbEner             0.0010134        0.015126       0.0032846       0.0033441
v  Dissip              9.2048e-05        0.031157      0.00045144      0.00039022
v  TurbVisc               0.16467          11.354          4.7129          5.2741
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              749:        0.90596E-01

===============================================================


 INSTANT    0.750000000E+03   TIME STEP NUMBER             750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001022E+04
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 :  0.23793E+00 0.13259E+01
   Friction velocity        uet   :  0.14235E-01 0.79027E-01
   Friction velocity        uk    :  0.17436E-01 0.38778E-01
   Dimensionless distance   yplus :  0.42840E+03 0.95270E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        750, Physical time    0.75000E+03


   ** 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:    0.73746E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62583E+01      54   0.14355E-02   0.20517E-01 
c  VelocityX    0.46300E+04      13   0.76510E-02   0.34808E-03 
c  VelocityY    0.46300E+04      13   0.76510E-02   0.27494E-04 
c  VelocityZ    0.46300E+04      13   0.76510E-02   0.56268E-04 
c  TurbEner     0.59762E+01      13   0.76375E-04   0.91140E-09 
c  Dissip       0.15103E+01      15   0.78987E-03   0.15961E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.9           54517           26776           27271
v  Velocity[x]            0.29288          2.1829         0.90809         0.90986
v  Velocity[y]           -0.38271         0.69398      0.00053912      0.00031963
v  Velocity[z]           -0.42108         0.51385      -0.0012542      -0.0013708
v  TurbEner             0.0010105        0.015197       0.0032846       0.0033441
v  Dissip              9.2075e-05        0.031345      0.00045164      0.00039034
v  TurbVisc               0.16526          11.338          4.7128          5.2741
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              750:        0.97165E-01

===============================================================


 INSTANT    0.751000000E+03   TIME STEP NUMBER             751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998847E+04
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 :  0.23783E+00 0.12361E+01
   Friction velocity        uet   :  0.14229E-01 0.72330E-01
   Friction velocity        uk    :  0.17412E-01 0.38687E-01
   Dimensionless distance   yplus :  0.42804E+03 0.95301E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72591E+01      62   0.15389E-02   0.23797E-01 
c  VelocityX    0.46299E+04      12   0.73124E-02   0.43316E-03 
c  VelocityY    0.46299E+04      12   0.73124E-02   0.68681E-04 
c  VelocityZ    0.46299E+04      12   0.73124E-02   0.12395E-03 
c  TurbEner     0.59777E+01      13   0.74555E-04   0.10230E-08 
c  Dissip       0.15394E+01      15   0.86213E-03   0.15053E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.7           54538           26776           27271
v  Velocity[x]            0.29258          2.2147         0.90806         0.90983
v  Velocity[y]           -0.36647         0.70234      0.00056276      0.00034212
v  Velocity[z]           -0.42315         0.50795       -0.001243      -0.0013607
v  TurbEner             0.0010147        0.015392       0.0032849       0.0033443
v  Dissip              9.2051e-05        0.031866      0.00045191      0.00039052
v  TurbVisc               0.16507          11.355          4.7128          5.2741
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              751:        0.90752E-01

===============================================================


 INSTANT    0.752000000E+03   TIME STEP NUMBER             752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000298E+04
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 :  0.23738E+00 0.13245E+01
   Friction velocity        uet   :  0.14202E-01 0.78956E-01
   Friction velocity        uk    :  0.17448E-01 0.38734E-01
   Dimensionless distance   yplus :  0.42809E+03 0.95270E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.74088E+01      63   0.16724E-02   0.24299E-01 
c  VelocityX    0.46298E+04      12   0.66238E-02   0.92351E-03 
c  VelocityY    0.46298E+04      12   0.66238E-02   0.36249E-04 
c  VelocityZ    0.46298E+04      12   0.66238E-02   0.55880E-04 
c  TurbEner     0.59772E+01      14   0.23354E-03   0.34374E-08 
c  Dissip       0.15418E+01      17   0.41653E-02   0.17413E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.86           54507           26777           27271
v  Velocity[x]            0.29297          1.6211         0.90806         0.90983
v  Velocity[y]           -0.38268         0.69344      0.00054038      0.00032174
v  Velocity[z]           -0.41882         0.51208      -0.0012553      -0.0013713
v  TurbEner             0.0010169        0.016641       0.0032852       0.0033446
v  Dissip              9.2053e-05        0.035277      0.00045225      0.00039079
v  TurbVisc               0.16521          11.337          4.7129          5.2741
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              752:        0.90256E-01

===============================================================


 INSTANT    0.753000000E+03   TIME STEP NUMBER             753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000829E+04
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 :  0.23759E+00 0.12684E+01
   Friction velocity        uet   :  0.14214E-01 0.73728E-01
   Friction velocity        uk    :  0.17467E-01 0.38810E-01
   Dimensionless distance   yplus :  0.42898E+03 0.95191E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62052E+01      59   0.13839E-02   0.20348E-01 
c  VelocityX    0.46299E+04      13   0.69684E-02   0.32465E-03 
c  VelocityY    0.46299E+04      13   0.69684E-02   0.26223E-04 
c  VelocityZ    0.46299E+04      13   0.69684E-02   0.44448E-04 
c  TurbEner     0.59709E+01      16   0.53727E-03   0.16954E-07 
c  Dissip       0.13412E+01      19   0.10802E-01   0.92286E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.89           54512           26776           27270
v  Velocity[x]            0.29267          1.8024         0.90805         0.90982
v  Velocity[y]           -0.36816         0.70063      0.00054721      0.00032499
v  Velocity[z]           -0.42054         0.50493      -0.0012546      -0.0013717
v  TurbEner             0.0010159        0.013723       0.0032848       0.0033443
v  Dissip              9.2025e-05        0.027946      0.00045128      0.00039007
v  TurbVisc               0.16572           11.34           4.713          5.2742
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              753:        0.91039E-01

===============================================================


 INSTANT    0.754000000E+03   TIME STEP NUMBER             754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001167E+04
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 :  0.23772E+00 0.13250E+01
   Friction velocity        uet   :  0.14223E-01 0.78980E-01
   Friction velocity        uk    :  0.17458E-01 0.38801E-01
   Dimensionless distance   yplus :  0.42915E+03 0.95162E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61024E+01      57   0.14956E-02   0.20021E-01 
c  VelocityX    0.46299E+04      12   0.71046E-02   0.43266E-03 
c  VelocityY    0.46299E+04      12   0.71046E-02   0.25285E-04 
c  VelocityZ    0.46299E+04      12   0.71046E-02   0.43881E-04 
c  TurbEner     0.59689E+01      14   0.22426E-03   0.47892E-08 
c  Dissip       0.12658E+01      19   0.52023E-02   0.25964E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.21           54494           26777           27271
v  Velocity[x]            0.29268          1.9525         0.90807         0.90984
v  Velocity[y]           -0.38256         0.69202      0.00054391      0.00032681
v  Velocity[z]           -0.42047         0.51236       -0.001248      -0.0013651
v  TurbEner             0.0010188        0.012672       0.0032845        0.003344
v  Dissip              9.2054e-05        0.024807       0.0004504      0.00038947
v  TurbVisc               0.16572          11.323           4.713          5.2742
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              754:        0.90595E-01

===============================================================


 INSTANT    0.755000000E+03   TIME STEP NUMBER             755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997815E+04
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 :  0.23802E+00 0.12158E+01
   Friction velocity        uet   :  0.14241E-01 0.72474E-01
   Friction velocity        uk    :  0.17482E-01 0.38757E-01
   Dimensionless distance   yplus :  0.42882E+03 0.95150E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67756E+01      57   0.13485E-02   0.22200E-01 
c  VelocityX    0.46299E+04      12   0.67155E-02   0.38878E-03 
c  VelocityY    0.46299E+04      12   0.67155E-02   0.27203E-04 
c  VelocityZ    0.46299E+04      12   0.67155E-02   0.46031E-04 
c  TurbEner     0.59677E+01      14   0.10374E-03   0.19582E-08 
c  Dissip       0.12267E+01      18   0.26545E-02   0.87060E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.27           54506           26776           27271
v  Velocity[x]            0.29304           2.038         0.90806         0.90983
v  Velocity[y]           -0.36625         0.70059      0.00053742      0.00031769
v  Velocity[z]           -0.42082          0.5067      -0.0012517      -0.0013674
v  TurbEner             0.0010223        0.012431        0.003284       0.0033437
v  Dissip              9.2051e-05        0.023387      0.00044961      0.00038891
v  TurbVisc               0.16557          11.314           4.713          5.2743
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              755:        0.90270E-01

===============================================================


 INSTANT    0.756000000E+03   TIME STEP NUMBER             756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001225E+04
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 :  0.23766E+00 0.13227E+01
   Friction velocity        uet   :  0.14220E-01 0.78851E-01
   Friction velocity        uk    :  0.17512E-01 0.38725E-01
   Dimensionless distance   yplus :  0.43008E+03 0.95170E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64347E+01      57   0.14196E-02   0.21114E-01 
c  VelocityX    0.46300E+04      12   0.69133E-02   0.35197E-03 
c  VelocityY    0.46300E+04      12   0.69133E-02   0.29041E-04 
c  VelocityZ    0.46300E+04      12   0.69133E-02   0.12747E-03 
c  TurbEner     0.59679E+01      13   0.72042E-04   0.86813E-09 
c  Dissip       0.12088E+01      17   0.14351E-02   0.38601E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.76           54515           26777           27271
v  Velocity[x]            0.29261           2.102         0.90806         0.90983
v  Velocity[y]           -0.38237          0.6931      0.00054961       0.0003294
v  Velocity[z]           -0.42164         0.51114      -0.0012414      -0.0013645
v  TurbEner             0.0010197        0.012626       0.0032836       0.0033435
v  Dissip              9.2068e-05        0.022932      0.00044893      0.00038844
v  TurbVisc               0.16625          11.343          4.7131          5.2743
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              756:        0.89791E-01

===============================================================


 INSTANT    0.757000000E+03   TIME STEP NUMBER             757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998988E+04
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 :  0.23768E+00 0.12155E+01
   Friction velocity        uet   :  0.14222E-01 0.72466E-01
   Friction velocity        uk    :  0.17490E-01 0.38666E-01
   Dimensionless distance   yplus :  0.42985E+03 0.95200E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64787E+01      61   0.14347E-02   0.21241E-01 
c  VelocityX    0.46300E+04      13   0.71722E-02   0.37476E-03 
c  VelocityY    0.46300E+04      13   0.71722E-02   0.27309E-04 
c  VelocityZ    0.46300E+04      13   0.71722E-02   0.48892E-04 
c  TurbEner     0.59685E+01      13   0.86710E-04   0.13330E-08 
c  Dissip       0.12056E+01      16   0.55963E-03   0.95247E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.93           54508           26777           27271
v  Velocity[x]            0.29277          2.1427         0.90807         0.90984
v  Velocity[y]           -0.36792         0.70045       0.0005557      0.00033459
v  Velocity[z]           -0.42151         0.50414      -0.0012447      -0.0013624
v  TurbEner             0.0010231        0.012966       0.0032834       0.0033433
v  Dissip              9.2144e-05        0.022919      0.00044841      0.00038808
v  TurbVisc               0.16599          11.326          4.7131          5.2744
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              757:        0.90655E-01

===============================================================


 INSTANT    0.758000000E+03   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999797E+04
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 :  0.23778E+00 0.13250E+01
   Friction velocity        uet   :  0.14229E-01 0.78983E-01
   Friction velocity        uk    :  0.17519E-01 0.38731E-01
   Dimensionless distance   yplus :  0.42979E+03 0.95224E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60145E+01      64   0.11743E-02   0.19714E-01 
c  VelocityX    0.46300E+04      12   0.69324E-02   0.29395E-03 
c  VelocityY    0.46300E+04      12   0.69324E-02   0.58018E-04 
c  VelocityZ    0.46300E+04      12   0.69324E-02   0.70037E-04 
c  TurbEner     0.59696E+01      13   0.11239E-03   0.17134E-08 
c  Dissip       0.12201E+01      16   0.79747E-03   0.90479E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.11           54519           26777           27271
v  Velocity[x]            0.29278          2.1664         0.90804         0.90982
v  Velocity[y]           -0.38301         0.69481      0.00056297      0.00034108
v  Velocity[z]           -0.41994         0.51138      -0.0012361      -0.0013582
v  TurbEner             0.0010239        0.013506       0.0032835       0.0033434
v  Dissip              9.2201e-05        0.023471      0.00044814       0.0003879
v  TurbVisc               0.16597          11.317          4.7132          5.2744
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              758:        0.90368E-01

===============================================================


 INSTANT    0.759000000E+03   TIME STEP NUMBER             759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999446E+04
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 :  0.23737E+00 0.12518E+01
   Friction velocity        uet   :  0.14205E-01 0.73113E-01
   Friction velocity        uk    :  0.17526E-01 0.38773E-01
   Dimensionless distance   yplus :  0.43039E+03 0.95275E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58994E+01      53   0.13366E-02   0.19350E-01 
c  VelocityX    0.46301E+04      12   0.72090E-02   0.35391E-03 
c  VelocityY    0.46301E+04      12   0.72090E-02   0.24684E-04 
c  VelocityZ    0.46301E+04      12   0.72090E-02   0.39487E-04 
c  TurbEner     0.59718E+01      13   0.11393E-03   0.18329E-08 
c  Dissip       0.12503E+01      16   0.13322E-02   0.26618E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.98           54522           26777           27271
v  Velocity[x]            0.29277           2.203         0.90806         0.90984
v  Velocity[y]           -0.36658         0.70256      0.00055486      0.00033025
v  Velocity[z]           -0.41978         0.50611      -0.0012507      -0.0013709
v  TurbEner             0.0010216        0.014016       0.0032837       0.0033435
v  Dissip              9.2206e-05        0.024354      0.00044811      0.00038789
v  TurbVisc               0.16629          11.358          4.7135          5.2747
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              759:        0.89307E-01

===============================================================


 INSTANT    0.760000000E+03   TIME STEP NUMBER             760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999632E+04
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 :  0.23799E+00 0.13253E+01
   Friction velocity        uet   :  0.14243E-01 0.79003E-01
   Friction velocity        uk    :  0.17507E-01 0.38782E-01
   Dimensionless distance   yplus :  0.43037E+03 0.95311E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64196E+01      56   0.16370E-02   0.21054E-01 
c  VelocityX    0.46300E+04      12   0.71356E-02   0.47352E-03 
c  VelocityY    0.46300E+04      12   0.71356E-02   0.27135E-04 
c  VelocityZ    0.46300E+04      12   0.71356E-02   0.39339E-04 
c  TurbEner     0.59732E+01      14   0.15451E-03   0.27966E-08 
c  Dissip       0.12772E+01      17   0.24749E-02   0.73805E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.75           54504           26778           27272
v  Velocity[x]            0.29293          2.0292         0.90807         0.90984
v  Velocity[y]           -0.38226         0.69204      0.00056044      0.00034073
v  Velocity[z]           -0.42166         0.51112      -0.0012459      -0.0013663
v  TurbEner             0.0010225        0.014858        0.003284       0.0033437
v  Dissip               9.217e-05        0.026223      0.00044827      0.00038802
v  TurbVisc               0.16616          11.342          4.7137          5.2749
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              760:        0.89807E-01

===============================================================


 INSTANT    0.761000000E+03   TIME STEP NUMBER             761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998873E+04
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 :  0.23791E+00 0.12174E+01
   Friction velocity        uet   :  0.14238E-01 0.72570E-01
   Friction velocity        uk    :  0.17515E-01 0.38675E-01
   Dimensionless distance   yplus :  0.42979E+03 0.95298E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60615E+01      53   0.13457E-02   0.19870E-01 
c  VelocityX    0.46301E+04      13   0.70671E-02   0.38629E-03 
c  VelocityY    0.46301E+04      13   0.70671E-02   0.28153E-04 
c  VelocityZ    0.46301E+04      13   0.70671E-02   0.51792E-04 
c  TurbEner     0.59727E+01      13   0.93401E-04   0.16008E-08 
c  Dissip       0.12708E+01      16   0.10172E-02   0.18901E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.57           54513           26777           27272
v  Velocity[x]            0.29284          2.0998         0.90805         0.90983
v  Velocity[y]           -0.36701         0.69991      0.00055682      0.00033447
v  Velocity[z]           -0.42126         0.50489      -0.0012554      -0.0013753
v  TurbEner             0.0010241        0.014511       0.0032842       0.0033439
v  Dissip              9.2159e-05         0.02567       0.0004482      0.00038798
v  TurbVisc               0.16587          11.342           4.714          5.2751
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              761:        0.89647E-01

===============================================================


 INSTANT    0.762000000E+03   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001322E+04
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 :  0.23756E+00 0.13242E+01
   Friction velocity        uet   :  0.14218E-01 0.78928E-01
   Friction velocity        uk    :  0.17528E-01 0.38756E-01
   Dimensionless distance   yplus :  0.43070E+03 0.95366E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57836E+01      51   0.13535E-02   0.18970E-01 
c  VelocityX    0.46302E+04      12   0.68341E-02   0.32124E-03 
c  VelocityY    0.46302E+04      12   0.68341E-02   0.42775E-04 
c  VelocityZ    0.46302E+04      12   0.68341E-02   0.34956E-04 
c  TurbEner     0.59739E+01      13   0.72284E-04   0.91420E-09 
c  Dissip       0.12884E+01      15   0.59965E-03   0.91594E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.46           54517           26778           27272
v  Velocity[x]            0.29265          2.1463         0.90805         0.90983
v  Velocity[y]           -0.38242         0.69306      0.00054952      0.00032963
v  Velocity[z]           -0.42104         0.51181      -0.0012578      -0.0013781
v  TurbEner             0.0010193        0.014556       0.0032846       0.0033442
v  Dissip               9.215e-05        0.025883      0.00044835      0.00038809
v  TurbVisc                0.1664          11.374          4.7143          5.2754
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              762:        0.88632E-01

===============================================================


 INSTANT    0.763000000E+03   TIME STEP NUMBER             763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999164E+04
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 :  0.23789E+00 0.12499E+01
   Friction velocity        uet   :  0.14238E-01 0.73004E-01
   Friction velocity        uk    :  0.17486E-01 0.38748E-01
   Dimensionless distance   yplus :  0.43005E+03 0.95414E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63268E+01      59   0.14162E-02   0.20750E-01 
c  VelocityX    0.46302E+04      12   0.74470E-02   0.34247E-03 
c  VelocityY    0.46302E+04      12   0.74470E-02   0.23261E-04 
c  VelocityZ    0.46302E+04      12   0.74470E-02   0.29073E-04 
c  TurbEner     0.59755E+01      13   0.86377E-04   0.14689E-08 
c  Dissip       0.13247E+01      17   0.13819E-02   0.38817E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.69           54513           26778           27272
v  Velocity[x]            0.29288          2.1878         0.90807         0.90985
v  Velocity[y]           -0.36632         0.70166      0.00055633      0.00033535
v  Velocity[z]           -0.42131         0.50629      -0.0012533      -0.0013679
v  TurbEner             0.0010213        0.014813       0.0032849       0.0033444
v  Dissip              9.2116e-05        0.026661      0.00044868      0.00038833
v  TurbVisc               0.16601          11.354          4.7146          5.2757
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              763:        0.89794E-01

===============================================================


 INSTANT    0.764000000E+03   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998540E+04
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 :  0.23769E+00 0.13234E+01
   Friction velocity        uet   :  0.14226E-01 0.78882E-01
   Friction velocity        uk    :  0.17504E-01 0.38785E-01
   Dimensionless distance   yplus :  0.42963E+03 0.95392E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67251E+01      58   0.15459E-02   0.22053E-01 
c  VelocityX    0.46302E+04      12   0.68931E-02   0.43185E-03 
c  VelocityY    0.46302E+04      12   0.68931E-02   0.28375E-04 
c  VelocityZ    0.46302E+04      12   0.68931E-02   0.44383E-04 
c  TurbEner     0.59761E+01      13   0.12123E-03   0.19143E-08 
c  Dissip       0.13528E+01      17   0.22744E-02   0.67866E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.06           54509           26779           27273
v  Velocity[x]            0.29299           2.021         0.90806         0.90984
v  Velocity[y]           -0.38295         0.69412      0.00055178      0.00033032
v  Velocity[z]           -0.41882         0.51041      -0.0012619      -0.0013836
v  TurbEner             0.0010217        0.015465       0.0032853       0.0033448
v  Dissip              9.2056e-05        0.028416      0.00044911      0.00038863
v  TurbVisc               0.16595          11.344          4.7147          5.2758
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              764:        0.89672E-01

===============================================================


 INSTANT    0.765000000E+03   TIME STEP NUMBER             765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998616E+04
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 :  0.23748E+00 0.12165E+01
   Friction velocity        uet   :  0.14214E-01 0.72520E-01
   Friction velocity        uk    :  0.17507E-01 0.38811E-01
   Dimensionless distance   yplus :  0.43009E+03 0.95374E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62997E+01      57   0.13772E-02   0.20665E-01 
c  VelocityX    0.46304E+04      13   0.69444E-02   0.31856E-03 
c  VelocityY    0.46304E+04      13   0.69444E-02   0.33503E-04 
c  VelocityZ    0.46304E+04      13   0.69444E-02   0.64870E-04 
c  TurbEner     0.59751E+01      14   0.11019E-03   0.18155E-08 
c  Dissip       0.13381E+01      16   0.13583E-02   0.33310E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.66           54512           26778           27273
v  Velocity[x]            0.29286           2.093         0.90807         0.90984
v  Velocity[y]           -0.36757         0.70127      0.00054156      0.00031865
v  Velocity[z]           -0.42001         0.50413      -0.0012579      -0.0013752
v  TurbEner             0.0010198        0.014969       0.0032853       0.0033448
v  Dissip              9.2076e-05        0.027629       0.0004491      0.00038862
v  TurbVisc               0.16637          11.377           4.715          5.2761
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              765:        0.90026E-01

===============================================================


 INSTANT    0.766000000E+03   TIME STEP NUMBER             766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000126E+04
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 :  0.23785E+00 0.13256E+01
   Friction velocity        uet   :  0.14237E-01 0.79014E-01
   Friction velocity        uk    :  0.17491E-01 0.38837E-01
   Dimensionless distance   yplus :  0.42997E+03 0.95384E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66309E+01      55   0.14793E-02   0.21742E-01 
c  VelocityX    0.46303E+04      12   0.66250E-02   0.36351E-03 
c  VelocityY    0.46303E+04      12   0.66250E-02   0.44591E-04 
c  VelocityZ    0.46303E+04      12   0.66250E-02   0.10799E-03 
c  TurbEner     0.59761E+01      13   0.67518E-04   0.81559E-09 
c  Dissip       0.13608E+01      15   0.55904E-03   0.90175E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.89           54527           26779           27273
v  Velocity[x]            0.29253          2.1497         0.90807         0.90985
v  Velocity[y]           -0.38247         0.69465      0.00056531      0.00034529
v  Velocity[z]            -0.4222         0.51174      -0.0012382      -0.0013608
v  TurbEner             0.0010224        0.014943       0.0032856       0.0033449
v  Dissip              9.2037e-05        0.027778      0.00044931      0.00038875
v  TurbVisc               0.16642           11.36          4.7151          5.2761
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              766:        0.89409E-01

===============================================================


 INSTANT    0.767000000E+03   TIME STEP NUMBER             767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999546E+04
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 :  0.23761E+00 0.12135E+01
   Friction velocity        uet   :  0.14222E-01 0.72334E-01
   Friction velocity        uk    :  0.17513E-01 0.38836E-01
   Dimensionless distance   yplus :  0.42953E+03 0.95291E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56046E+01      55   0.12582E-02   0.18382E-01 
c  VelocityX    0.46304E+04      12   0.68446E-02   0.34633E-03 
c  VelocityY    0.46304E+04      12   0.68446E-02   0.28633E-04 
c  VelocityZ    0.46304E+04      12   0.68446E-02   0.42377E-04 
c  TurbEner     0.59770E+01      13   0.81845E-04   0.12258E-08 
c  Dissip       0.13920E+01      16   0.12784E-02   0.34972E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -174.8           54527           26779           27273
v  Velocity[x]            0.29286           2.178         0.90805         0.90982
v  Velocity[y]           -0.36624         0.70235      0.00055499      0.00032971
v  Velocity[z]           -0.42004         0.50635      -0.0012499      -0.0013688
v  TurbEner             0.0010261        0.015152       0.0032861       0.0033453
v  Dissip              9.2051e-05        0.028484      0.00044974      0.00038904
v  TurbVisc               0.16643          11.366          4.7153          5.2763
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              767:        0.89399E-01

===============================================================


 INSTANT    0.768000000E+03   TIME STEP NUMBER             768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998461E+04
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 :  0.23788E+00 0.13252E+01
   Friction velocity        uet   :  0.14238E-01 0.78989E-01
   Friction velocity        uk    :  0.17545E-01 0.38865E-01
   Dimensionless distance   yplus :  0.43070E+03 0.95272E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58089E+01      52   0.13201E-02   0.19047E-01 
c  VelocityX    0.46304E+04      12   0.69651E-02   0.31362E-03 
c  VelocityY    0.46304E+04      12   0.69651E-02   0.28555E-04 
c  VelocityZ    0.46304E+04      12   0.69651E-02   0.40814E-04 
c  TurbEner     0.59788E+01      13   0.79606E-04   0.97507E-09 
c  Dissip       0.14290E+01      16   0.12686E-02   0.33397E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -167.6           54527           26780           27274
v  Velocity[x]            0.29279          2.2045         0.90806         0.90984
v  Velocity[y]            -0.3824         0.69221      0.00055209      0.00032773
v  Velocity[z]           -0.42153         0.51096      -0.0012534      -0.0013713
v  TurbEner             0.0010247        0.015345       0.0032865       0.0033456
v  Dissip              9.2042e-05        0.029239       0.0004502      0.00038935
v  TurbVisc               0.16728          11.343          4.7156          5.2765
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              768:        0.89181E-01

===============================================================


 INSTANT    0.769000000E+03   TIME STEP NUMBER             769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998027E+04
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 :  0.23775E+00 0.12172E+01
   Friction velocity        uet   :  0.14231E-01 0.72550E-01
   Friction velocity        uk    :  0.17533E-01 0.38763E-01
   Dimensionless distance   yplus :  0.43067E+03 0.95314E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60842E+01      57   0.13465E-02   0.19946E-01 
c  VelocityX    0.46304E+04      12   0.70291E-02   0.42022E-03 
c  VelocityY    0.46304E+04      12   0.70291E-02   0.38648E-04 
c  VelocityZ    0.46304E+04      12   0.70291E-02   0.34947E-04 
c  TurbEner     0.59799E+01      13   0.13514E-03   0.15188E-08 
c  Dissip       0.14584E+01      17   0.25153E-02   0.79302E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.62           54538           26779           27273
v  Velocity[x]            0.29289          2.0295         0.90807         0.90984
v  Velocity[y]             -0.368         0.69993       0.0005544      0.00033112
v  Velocity[z]           -0.42217         0.50405      -0.0012659      -0.0013825
v  TurbEner             0.0010301        0.016044        0.003287        0.003346
v  Dissip              9.2079e-05        0.031282      0.00045071      0.00038971
v  TurbVisc               0.16735          11.338          4.7158          5.2768
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              769:        0.89719E-01

===============================================================


 INSTANT    0.770000000E+03   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001506E+04
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 :  0.23767E+00 0.13241E+01
   Friction velocity        uet   :  0.14226E-01 0.78923E-01
   Friction velocity        uk    :  0.17579E-01 0.38783E-01
   Dimensionless distance   yplus :  0.43099E+03 0.95287E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54871E+01      56   0.11666E-02   0.17986E-01 
c  VelocityX    0.46304E+04      12   0.64928E-02   0.34200E-03 
c  VelocityY    0.46304E+04      12   0.64928E-02   0.24641E-04 
c  VelocityZ    0.46304E+04      12   0.64928E-02   0.43838E-04 
c  TurbEner     0.59794E+01      13   0.13825E-03   0.20568E-08 
c  Dissip       0.14390E+01      16   0.16018E-02   0.43257E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.75           54550           26779           27273
v  Velocity[x]            0.29293          2.1044         0.90806         0.90984
v  Velocity[y]           -0.38305         0.69482      0.00054289      0.00032133
v  Velocity[z]           -0.41907         0.51128      -0.0012562      -0.0013758
v  TurbEner             0.0010335        0.015391       0.0032873       0.0033463
v  Dissip              9.2102e-05        0.030239      0.00045082       0.0003898
v  TurbVisc               0.16773          11.368           4.716           5.277
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              770:        0.89126E-01

===============================================================


 INSTANT    0.771000000E+03   TIME STEP NUMBER             771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000466E+04
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 :  0.23747E+00 0.12345E+01
   Friction velocity        uet   :  0.14214E-01 0.72318E-01
   Friction velocity        uk    :  0.17608E-01 0.38815E-01
   Dimensionless distance   yplus :  0.43215E+03 0.95326E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64542E+01      53   0.14770E-02   0.21174E-01 
c  VelocityX    0.46305E+04      13   0.67432E-02   0.29276E-03 
c  VelocityY    0.46305E+04      13   0.67432E-02   0.24294E-04 
c  VelocityZ    0.46305E+04      13   0.67432E-02   0.68152E-04 
c  TurbEner     0.59799E+01      13   0.62656E-04   0.79023E-09 
c  Dissip       0.14600E+01      14   0.37647E-03   0.42938E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.31           54541           26779           27273
v  Velocity[x]             0.2927          2.1589         0.90806         0.90983
v  Velocity[y]           -0.36819         0.70327      0.00054886      0.00032653
v  Velocity[z]           -0.42018         0.50696      -0.0012489      -0.0013683
v  TurbEner             0.0010336        0.015291       0.0032875       0.0033465
v  Dissip              9.2072e-05         0.03038      0.00045107      0.00038997
v  TurbVisc               0.16851           11.35          4.7162          5.2772
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              771:        0.89547E-01

===============================================================


 INSTANT    0.772000000E+03   TIME STEP NUMBER             772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999706E+04
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 :  0.23769E+00 0.13243E+01
   Friction velocity        uet   :  0.14228E-01 0.78940E-01
   Friction velocity        uk    :  0.17609E-01 0.38849E-01
   Dimensionless distance   yplus :  0.43255E+03 0.95359E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66846E+01      63   0.16453E-02   0.21931E-01 
c  VelocityX    0.46304E+04      13   0.74523E-02   0.37090E-03 
c  VelocityY    0.46304E+04      13   0.74523E-02   0.30655E-04 
c  VelocityZ    0.46304E+04      13   0.74523E-02   0.50444E-04 
c  TurbEner     0.59812E+01      13   0.75502E-04   0.12500E-08 
c  Dissip       0.14906E+01      16   0.11757E-02   0.30161E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -168           54521           26780           27274
v  Velocity[x]            0.29283          2.1721         0.90808         0.90986
v  Velocity[y]           -0.38282         0.69115      0.00055523      0.00033479
v  Velocity[z]           -0.42077         0.51388      -0.0012442      -0.0013649
v  TurbEner             0.0010376         0.01548       0.0032879       0.0033468
v  Dissip              9.2081e-05        0.031051      0.00045147      0.00039025
v  TurbVisc               0.16875          11.364          4.7162          5.2772
v  total_pressure           83077      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              772:        0.91224E-01

===============================================================


 INSTANT    0.773000000E+03   TIME STEP NUMBER             773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998338E+04
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 :  0.23793E+00 0.12420E+01
   Friction velocity        uet   :  0.14242E-01 0.72560E-01
   Friction velocity        uk    :  0.17643E-01 0.38867E-01
   Dimensionless distance   yplus :  0.43251E+03 0.95305E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67622E+01      60   0.13373E-02   0.22160E-01 
c  VelocityX    0.46305E+04      12   0.69567E-02   0.41903E-03 
c  VelocityY    0.46305E+04      12   0.69567E-02   0.40252E-04 
c  VelocityZ    0.46305E+04      12   0.69567E-02   0.34033E-04 
c  TurbEner     0.59817E+01      13   0.74246E-04   0.10664E-08 
c  Dissip       0.15225E+01      16   0.10114E-02   0.23599E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.47           54528           26779           27273
v  Velocity[x]            0.29307          2.2106         0.90805         0.90982
v  Velocity[y]            -0.3665         0.70052      0.00055791      0.00033248
v  Velocity[z]            -0.4201         0.50794      -0.0012388      -0.0013578
v  TurbEner             0.0010425        0.015574       0.0032882       0.0033471
v  Dissip              9.2095e-05        0.031587      0.00045192      0.00039056
v  TurbVisc               0.16889          11.341          4.7162          5.2773
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              773:        0.90471E-01

===============================================================


 INSTANT    0.774000000E+03   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002738E+04
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 :  0.23770E+00 0.13235E+01
   Friction velocity        uet   :  0.14228E-01 0.78885E-01
   Friction velocity        uk    :  0.17684E-01 0.38766E-01
   Dimensionless distance   yplus :  0.43407E+03 0.95290E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67546E+01      61   0.15306E-02   0.22173E-01 
c  VelocityX    0.46304E+04      12   0.64476E-02   0.41256E-03 
c  VelocityY    0.46304E+04      12   0.64476E-02   0.46255E-04 
c  VelocityZ    0.46304E+04      12   0.64476E-02   0.45399E-04 
c  TurbEner     0.59821E+01      13   0.12514E-03   0.16312E-08 
c  Dissip       0.15445E+01      16   0.22407E-02   0.62450E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.28           54537           26779           27274
v  Velocity[x]            0.29254          2.0281         0.90806         0.90985
v  Velocity[y]           -0.38268         0.69438      0.00054324      0.00032152
v  Velocity[z]            -0.4222         0.51217       -0.001261      -0.0013791
v  TurbEner             0.0010409        0.016202       0.0032884       0.0033473
v  Dissip              9.2122e-05        0.033402      0.00045238      0.00039089
v  TurbVisc               0.16985          11.344          4.7163          5.2774
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              774:        0.90493E-01

===============================================================


 INSTANT    0.775000000E+03   TIME STEP NUMBER             775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998283E+04
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 :  0.23760E+00 0.12552E+01
   Friction velocity        uet   :  0.14223E-01 0.73287E-01
   Friction velocity        uk    :  0.17671E-01 0.38682E-01
   Dimensionless distance   yplus :  0.43406E+03 0.95231E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63858E+01      63   0.12555E-02   0.20937E-01 
c  VelocityX    0.46303E+04      12   0.68296E-02   0.35079E-03 
c  VelocityY    0.46303E+04      12   0.68296E-02   0.40583E-04 
c  VelocityZ    0.46303E+04      12   0.68296E-02   0.10555E-03 
c  TurbEner     0.59809E+01      14   0.13496E-03   0.20871E-08 
c  Dissip       0.15188E+01      16   0.18521E-02   0.58858E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.42           54545           26779           27273
v  Velocity[x]            0.29248          2.1095         0.90803         0.90981
v  Velocity[y]           -0.36827         0.70278      0.00055375      0.00032974
v  Velocity[z]           -0.42225         0.50492      -0.0012508      -0.0013705
v  TurbEner             0.0010459        0.015618       0.0032883       0.0033472
v  Dissip               9.213e-05        0.032225      0.00045239       0.0003909
v  TurbVisc                0.1698          11.323          4.7162          5.2773
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              775:        0.90692E-01

===============================================================


 INSTANT    0.776000000E+03   TIME STEP NUMBER             776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001465E+04
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 :  0.23787E+00 0.13236E+01
   Friction velocity        uet   :  0.14239E-01 0.78899E-01
   Friction velocity        uk    :  0.17713E-01 0.38702E-01
   Dimensionless distance   yplus :  0.43428E+03 0.95132E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62455E+01      53   0.12590E-02   0.20481E-01 
c  VelocityX    0.46303E+04      12   0.70678E-02   0.30068E-03 
c  VelocityY    0.46303E+04      12   0.70678E-02   0.41755E-04 
c  VelocityZ    0.46303E+04      12   0.70678E-02   0.50683E-04 
c  TurbEner     0.59812E+01      12   0.60464E-04   0.55813E-09 
c  Dissip       0.15293E+01      14   0.36695E-03   0.39097E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.32           54554           26779           27273
v  Velocity[x]            0.29329          2.1476         0.90805         0.90984
v  Velocity[y]           -0.38252         0.69532      0.00054613      0.00032435
v  Velocity[z]           -0.41945         0.51231      -0.0012498      -0.0013712
v  TurbEner             0.0010484        0.015542       0.0032885       0.0033473
v  Dissip              9.2173e-05        0.032194      0.00045261      0.00039105
v  TurbVisc               0.17001          11.322          4.7161          5.2773
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              776:        0.89063E-01

===============================================================


 INSTANT    0.777000000E+03   TIME STEP NUMBER             777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000210E+04
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 :  0.23746E+00 0.12678E+01
   Friction velocity        uet   :  0.14214E-01 0.73804E-01
   Friction velocity        uk    :  0.17735E-01 0.38755E-01
   Dimensionless distance   yplus :  0.43528E+03 0.95107E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60933E+01      55   0.12402E-02   0.19977E-01 
c  VelocityX    0.46303E+04      12   0.70410E-02   0.33542E-03 
c  VelocityY    0.46303E+04      12   0.70410E-02   0.31639E-04 
c  VelocityZ    0.46303E+04      12   0.70410E-02   0.28366E-04 
c  TurbEner     0.59824E+01      12   0.69285E-04   0.69516E-09 
c  Dissip       0.15571E+01      15   0.86550E-03   0.18629E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.89           54557           26778           27273
v  Velocity[x]             0.2927          2.1913         0.90806         0.90983
v  Velocity[y]           -0.36621         0.70102       0.0005479      0.00032452
v  Velocity[z]           -0.42044         0.50685      -0.0012588      -0.0013776
v  TurbEner             0.0010473        0.015564       0.0032886       0.0033475
v  Dissip              9.2163e-05        0.032533      0.00045294      0.00039128
v  TurbVisc               0.17056           11.35          4.7161          5.2773
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              777:        0.89327E-01

===============================================================


 INSTANT    0.778000000E+03   TIME STEP NUMBER             778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000194E+04
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 :  0.23781E+00 0.13257E+01
   Friction velocity        uet   :  0.14235E-01 0.79015E-01
   Friction velocity        uk    :  0.17726E-01 0.38788E-01
   Dimensionless distance   yplus :  0.43550E+03 0.95098E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61623E+01      54   0.14904E-02   0.20205E-01 
c  VelocityX    0.46303E+04      12   0.73839E-02   0.41452E-03 
c  VelocityY    0.46303E+04      12   0.73839E-02   0.25768E-04 
c  VelocityZ    0.46303E+04      12   0.73839E-02   0.46008E-04 
c  TurbEner     0.59827E+01      13   0.10358E-03   0.10587E-08 
c  Dissip       0.15709E+01      16   0.19555E-02   0.45598E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.98           54549           26779           27273
v  Velocity[x]            0.29244          2.0205         0.90808         0.90986
v  Velocity[y]           -0.38251         0.69229      0.00054129      0.00032158
v  Velocity[z]           -0.42207          0.5112      -0.0012566      -0.0013759
v  TurbEner             0.0010496        0.016059       0.0032889       0.0033477
v  Dissip              9.2153e-05        0.034104      0.00045328      0.00039153
v  TurbVisc               0.17053          11.332           4.716          5.2772
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              778:        0.89536E-01

===============================================================


 INSTANT    0.779000000E+03   TIME STEP NUMBER             779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998460E+04
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 :  0.23786E+00 0.12161E+01
   Friction velocity        uet   :  0.14237E-01 0.72488E-01
   Friction velocity        uk    :  0.17745E-01 0.38763E-01
   Dimensionless distance   yplus :  0.43507E+03 0.95028E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65419E+01      65   0.15843E-02   0.21443E-01 
c  VelocityX    0.46302E+04      12   0.67852E-02   0.40952E-03 
c  VelocityY    0.46302E+04      12   0.67852E-02   0.35309E-04 
c  VelocityZ    0.46302E+04      12   0.67852E-02   0.10290E-03 
c  TurbEner     0.59816E+01      14   0.15172E-03   0.26700E-08 
c  Dissip       0.15375E+01      16   0.21799E-02   0.75563E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.86           54521           26778           27272
v  Velocity[x]            0.29295          2.0934         0.90804         0.90982
v  Velocity[y]            -0.3681         0.70016      0.00055162      0.00033016
v  Velocity[z]           -0.42176          0.5041      -0.0012402      -0.0013602
v  TurbEner             0.0010516        0.015405       0.0032889       0.0033477
v  Dissip              9.2146e-05        0.032691      0.00045317      0.00039147
v  TurbVisc               0.17024          11.336           4.716          5.2772
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              779:        0.91407E-01

===============================================================


 INSTANT    0.780000000E+03   TIME STEP NUMBER             780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000998E+04
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 :  0.23741E+00 0.13227E+01
   Friction velocity        uet   :  0.14209E-01 0.78837E-01
   Friction velocity        uk    :  0.17761E-01 0.38658E-01
   Dimensionless distance   yplus :  0.43604E+03 0.95078E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57267E+01      60   0.12094E-02   0.18792E-01 
c  VelocityX    0.46302E+04      12   0.64922E-02   0.34171E-03 
c  VelocityY    0.46302E+04      12   0.64922E-02   0.27863E-04 
c  VelocityZ    0.46302E+04      12   0.64922E-02   0.46168E-04 
c  TurbEner     0.59810E+01      13   0.71781E-04   0.10571E-08 
c  Dissip       0.15430E+01      14   0.47061E-03   0.42304E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.11           54532           26779           27273
v  Velocity[x]            0.29281          2.1433         0.90805         0.90983
v  Velocity[y]           -0.38289         0.69277      0.00054396      0.00032237
v  Velocity[z]           -0.42158         0.51157      -0.0012516      -0.0013715
v  TurbEner             0.0010471        0.015235       0.0032888       0.0033477
v  Dissip              9.2158e-05        0.032441      0.00045318      0.00039147
v  TurbVisc               0.17066          11.372           4.716          5.2772
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              780:        0.90222E-01

===============================================================


 INSTANT    0.781000000E+03   TIME STEP NUMBER             781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999154E+04
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 :  0.23802E+00 0.12151E+01
   Friction velocity        uet   :  0.14245E-01 0.72436E-01
   Friction velocity        uk    :  0.17724E-01 0.38670E-01
   Dimensionless distance   yplus :  0.43550E+03 0.95101E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61682E+01      57   0.13129E-02   0.20215E-01 
c  VelocityX    0.46302E+04      12   0.73290E-02   0.38732E-03 
c  VelocityY    0.46302E+04      12   0.73290E-02   0.24376E-04 
c  VelocityZ    0.46302E+04      12   0.73290E-02   0.32232E-04 
c  TurbEner     0.59815E+01      13   0.74094E-04   0.85353E-09 
c  Dissip       0.15644E+01      15   0.70917E-03   0.12777E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -177.8           54529           26778           27272
v  Velocity[x]            0.29272          2.1821         0.90806         0.90984
v  Velocity[y]           -0.36809         0.70046       0.0005569      0.00033564
v  Velocity[z]           -0.42166         0.50707       -0.001256      -0.0013755
v  TurbEner             0.0010487        0.015225       0.0032887       0.0033476
v  Dissip              9.2159e-05        0.032641      0.00045332      0.00039156
v  TurbVisc               0.17011          11.352          4.7159          5.2771
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              781:        0.88454E-01

===============================================================


 INSTANT    0.782000000E+03   TIME STEP NUMBER             782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001780E+04
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 :  0.23776E+00 0.13246E+01
   Friction velocity        uet   :  0.14228E-01 0.78958E-01
   Friction velocity        uk    :  0.17737E-01 0.38726E-01
   Dimensionless distance   yplus :  0.43518E+03 0.95109E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64577E+01      58   0.17065E-02   0.21175E-01 
c  VelocityX    0.46301E+04      12   0.74534E-02   0.40659E-03 
c  VelocityY    0.46301E+04      12   0.74534E-02   0.26741E-04 
c  VelocityZ    0.46301E+04      12   0.74534E-02   0.47726E-04 
c  TurbEner     0.59814E+01      13   0.10825E-03   0.14177E-08 
c  Dissip       0.15732E+01      15   0.17838E-02   0.35396E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.91           54507           26778           27272
v  Velocity[x]            0.29305          2.0147         0.90807         0.90985
v  Velocity[y]           -0.38288         0.69403      0.00055488      0.00033651
v  Velocity[z]           -0.41894         0.51386      -0.0012527       -0.001372
v  TurbEner             0.0010477        0.015679       0.0032888       0.0033477
v  Dissip              9.2199e-05        0.034053      0.00045354      0.00039173
v  TurbVisc               0.16982          11.354          4.7157          5.2769
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              782:        0.89410E-01

===============================================================


 INSTANT    0.783000000E+03   TIME STEP NUMBER             783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999528E+04
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 :  0.23736E+00 0.12140E+01
   Friction velocity        uet   :  0.14203E-01 0.72325E-01
   Friction velocity        uk    :  0.17728E-01 0.38758E-01
   Dimensionless distance   yplus :  0.43549E+03 0.95134E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63926E+01      58   0.14084E-02   0.20961E-01 
c  VelocityX    0.46301E+04      12   0.66575E-02   0.37041E-03 
c  VelocityY    0.46301E+04      12   0.66575E-02   0.57599E-04 
c  VelocityZ    0.46301E+04      12   0.66575E-02   0.12850E-03 
c  TurbEner     0.59792E+01      14   0.16183E-03   0.31970E-08 
c  Dissip       0.15334E+01      17   0.24960E-02   0.92371E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.14           54516           26777           27271
v  Velocity[x]            0.29259          2.0907         0.90804         0.90981
v  Velocity[y]           -0.36664         0.70211       0.0005621      0.00033916
v  Velocity[z]           -0.42013         0.50785       -0.001251      -0.0013719
v  TurbEner             0.0010432        0.015019       0.0032886       0.0033474
v  Dissip              9.2184e-05        0.032446      0.00045326      0.00039153
v  TurbVisc               0.16984          11.329          4.7156          5.2768
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              783:        0.90090E-01

===============================================================


 INSTANT    0.784000000E+03   TIME STEP NUMBER             784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002242E+04
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 :  0.23779E+00 0.13253E+01
   Friction velocity        uet   :  0.14228E-01 0.79004E-01
   Friction velocity        uk    :  0.17690E-01 0.38733E-01
   Dimensionless distance   yplus :  0.43499E+03 0.95145E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57424E+01      54   0.13819E-02   0.18826E-01 
c  VelocityX    0.46300E+04      12   0.71998E-02   0.34679E-03 
c  VelocityY    0.46300E+04      12   0.71998E-02   0.30564E-04 
c  VelocityZ    0.46300E+04      12   0.71998E-02   0.54739E-04 
c  TurbEner     0.59792E+01      13   0.70459E-04   0.84402E-09 
c  Dissip       0.15333E+01      14   0.57755E-03   0.51355E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.68           54521           26777           27272
v  Velocity[x]            0.29281          2.1397         0.90807         0.90985
v  Velocity[y]           -0.38274         0.69211      0.00055083      0.00033121
v  Velocity[z]           -0.42256         0.51208      -0.0012524      -0.0013725
v  TurbEner             0.0010421        0.014894       0.0032884       0.0033473
v  Dissip              9.2157e-05        0.032106      0.00045314      0.00039145
v  TurbVisc               0.16932          11.329          4.7154          5.2766
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              784:        0.89454E-01

===============================================================


 INSTANT    0.785000000E+03   TIME STEP NUMBER             785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999039E+04
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 :  0.23775E+00 0.12235E+01
   Friction velocity        uet   :  0.14224E-01 0.72523E-01
   Friction velocity        uk    :  0.17681E-01 0.38630E-01
   Dimensionless distance   yplus :  0.43395E+03 0.95147E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62183E+01      55   0.13829E-02   0.20387E-01 
c  VelocityX    0.46300E+04      13   0.72759E-02   0.38185E-03 
c  VelocityY    0.46300E+04      13   0.72759E-02   0.25260E-04 
c  VelocityZ    0.46300E+04      13   0.72759E-02   0.37292E-04 
c  TurbEner     0.59801E+01      13   0.64915E-04   0.83770E-09 
c  Dissip       0.15492E+01      14   0.58168E-03   0.86273E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.48           54503           26777           27271
v  Velocity[x]            0.29308          2.1811         0.90805         0.90982
v  Velocity[y]           -0.36802         0.70049      0.00055684      0.00033567
v  Velocity[z]           -0.42038         0.50507      -0.0012477      -0.0013662
v  TurbEner             0.0010414         0.01491       0.0032884       0.0033474
v  Dissip              9.2103e-05        0.032204      0.00045327      0.00039154
v  TurbVisc               0.16866          11.304          4.7152          5.2764
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              785:        0.89960E-01

===============================================================


 INSTANT    0.786000000E+03   TIME STEP NUMBER             786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001418E+04
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 :  0.23778E+00 0.13240E+01
   Friction velocity        uet   :  0.14224E-01 0.78926E-01
   Friction velocity        uk    :  0.17676E-01 0.38582E-01
   Dimensionless distance   yplus :  0.43440E+03 0.95196E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55408E+01      53   0.12984E-02   0.18175E-01 
c  VelocityX    0.46300E+04      12   0.69492E-02   0.39132E-03 
c  VelocityY    0.46300E+04      12   0.69492E-02   0.22046E-04 
c  VelocityZ    0.46300E+04      12   0.69492E-02   0.47740E-04 
c  TurbEner     0.59796E+01      13   0.10848E-03   0.14642E-08 
c  Dissip       0.15545E+01      15   0.16945E-02   0.30112E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.7           54510           26777           27271
v  Velocity[x]             0.2927          2.0136         0.90805         0.90983
v  Velocity[y]           -0.38263         0.69589      0.00054481      0.00032535
v  Velocity[z]           -0.42122         0.51233      -0.0012627      -0.0013822
v  TurbEner             0.0010345        0.015387       0.0032884       0.0033473
v  Dissip              9.2117e-05        0.033529      0.00045335      0.00039162
v  TurbVisc                0.1688          11.308           4.715          5.2763
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              786:        0.88987E-01

===============================================================


 INSTANT    0.787000000E+03   TIME STEP NUMBER             787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998247E+04
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 :  0.23785E+00 0.12384E+01
   Friction velocity        uet   :  0.14227E-01 0.72336E-01
   Friction velocity        uk    :  0.17617E-01 0.38651E-01
   Dimensionless distance   yplus :  0.43333E+03 0.95204E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69490E+01      56   0.16218E-02   0.22783E-01 
c  VelocityX    0.46299E+04      12   0.70058E-02   0.39555E-03 
c  VelocityY    0.46299E+04      12   0.70058E-02   0.43839E-04 
c  VelocityZ    0.46299E+04      12   0.70058E-02   0.11830E-03 
c  TurbEner     0.59781E+01      14   0.14497E-03   0.19671E-08 
c  Dissip       0.15135E+01      17   0.26562E-02   0.96338E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.57           54522           26776           27270
v  Velocity[x]            0.29276          2.0945         0.90805         0.90982
v  Velocity[y]           -0.36668         0.70412      0.00056109      0.00033873
v  Velocity[z]           -0.42318         0.50641      -0.0012516      -0.0013711
v  TurbEner              0.001034        0.014761        0.003288        0.003347
v  Dissip              9.2098e-05        0.031797        0.000453      0.00039138
v  TurbVisc               0.16798          11.312          4.7149          5.2761
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              787:        0.89776E-01

===============================================================


 INSTANT    0.788000000E+03   TIME STEP NUMBER             788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001300E+04
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 :  0.23754E+00 0.13252E+01
   Friction velocity        uet   :  0.14208E-01 0.78994E-01
   Friction velocity        uk    :  0.17612E-01 0.38738E-01
   Dimensionless distance   yplus :  0.43244E+03 0.95213E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73354E+01      70   0.16679E-02   0.24045E-01 
c  VelocityX    0.46298E+04      12   0.67002E-02   0.41780E-03 
c  VelocityY    0.46298E+04      12   0.67002E-02   0.67567E-04 
c  VelocityZ    0.46298E+04      12   0.67002E-02   0.60935E-04 
c  TurbEner     0.59781E+01      13   0.75681E-04   0.11669E-08 
c  Dissip       0.15018E+01      14   0.85539E-03   0.87217E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -165.8           54507           26777           27271
v  Velocity[x]            0.29272          2.1382         0.90806         0.90985
v  Velocity[y]           -0.38227         0.69207      0.00055299      0.00033276
v  Velocity[z]           -0.41913          0.5114      -0.0012509      -0.0013702
v  TurbEner             0.0010309        0.014661       0.0032878        0.003347
v  Dissip              9.2041e-05        0.031205      0.00045286      0.00039128
v  TurbVisc               0.16749           11.36          4.7146          5.2758
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              788:        0.91920E-01

===============================================================


 INSTANT    0.789000000E+03   TIME STEP NUMBER             789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999276E+04
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 :  0.23756E+00 0.12456E+01
   Friction velocity        uet   :  0.14208E-01 0.72714E-01
   Friction velocity        uk    :  0.17586E-01 0.38739E-01
   Dimensionless distance   yplus :  0.43220E+03 0.95239E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62992E+01      59   0.12151E-02   0.20657E-01 
c  VelocityX    0.46300E+04      12   0.64376E-02   0.30827E-03 
c  VelocityY    0.46300E+04      12   0.64376E-02   0.42280E-04 
c  VelocityZ    0.46300E+04      12   0.64376E-02   0.29773E-04 
c  TurbEner     0.59785E+01      13   0.68621E-04   0.99548E-09 
c  Dissip       0.15149E+01      14   0.48483E-03   0.59813E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.34           54511           26777           27271
v  Velocity[x]            0.29281          2.1834         0.90804         0.90981
v  Velocity[y]           -0.36702         0.70172      0.00055119      0.00032951
v  Velocity[z]           -0.42066         0.50487      -0.0012482      -0.0013675
v  TurbEner             0.0010257         0.01478       0.0032877       0.0033468
v  Dissip              9.2024e-05        0.031306      0.00045281      0.00039125
v  TurbVisc               0.16731          11.343          4.7144          5.2756
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              789:        0.89937E-01

===============================================================


 INSTANT    0.790000000E+03   TIME STEP NUMBER             790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000440E+04
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 :  0.23781E+00 0.13232E+01
   Friction velocity        uet   :  0.14223E-01 0.78872E-01
   Friction velocity        uk    :  0.17542E-01 0.38747E-01
   Dimensionless distance   yplus :  0.43149E+03 0.95306E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61918E+01      56   0.15331E-02   0.20306E-01 
c  VelocityX    0.46298E+04      12   0.71093E-02   0.37383E-03 
c  VelocityY    0.46298E+04      12   0.71093E-02   0.34047E-04 
c  VelocityZ    0.46298E+04      12   0.71093E-02   0.43531E-04 
c  TurbEner     0.59788E+01      13   0.12602E-03   0.13801E-08 
c  Dissip       0.15227E+01      16   0.18453E-02   0.35581E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -170.7           54517           26777           27272
v  Velocity[x]            0.29282          2.0102         0.90805         0.90983
v  Velocity[y]           -0.38247         0.69473      0.00054458       0.0003258
v  Velocity[z]           -0.42038         0.51193      -0.0012564       -0.001379
v  TurbEner             0.0010245        0.015381       0.0032875       0.0033467
v  Dissip              9.1982e-05        0.032739      0.00045285      0.00039128
v  TurbVisc               0.16676          11.348          4.7142          5.2754
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              790:        0.89857E-01

===============================================================


 INSTANT    0.791000000E+03   TIME STEP NUMBER             791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998952E+04
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 :  0.23819E+00 0.12554E+01
   Friction velocity        uet   :  0.14246E-01 0.73161E-01
   Friction velocity        uk    :  0.17531E-01 0.38758E-01
   Dimensionless distance   yplus :  0.43038E+03 0.95297E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66368E+01      56   0.14802E-02   0.21760E-01 
c  VelocityX    0.46299E+04      12   0.68515E-02   0.39895E-03 
c  VelocityY    0.46299E+04      12   0.68515E-02   0.37840E-04 
c  VelocityZ    0.46299E+04      12   0.68515E-02   0.11242E-03 
c  TurbEner     0.59775E+01      14   0.12807E-03   0.20714E-08 
c  Dissip       0.14882E+01      17   0.22837E-02   0.75160E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.29           54516           26777           27271
v  Velocity[x]            0.29301          2.0935         0.90804         0.90982
v  Velocity[y]           -0.36697         0.70297      0.00055524      0.00033401
v  Velocity[z]           -0.42106         0.50578      -0.0012349      -0.0013572
v  TurbEner             0.0010245        0.014846       0.0032872       0.0033465
v  Dissip              9.2014e-05        0.031284      0.00045253      0.00039108
v  TurbVisc               0.16621          11.322           4.714          5.2751
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              791:        0.89716E-01

===============================================================


 INSTANT    0.792000000E+03   TIME STEP NUMBER             792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000878E+04
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 :  0.23748E+00 0.13238E+01
   Friction velocity        uet   :  0.14204E-01 0.78900E-01
   Friction velocity        uk    :  0.17531E-01 0.38708E-01
   Dimensionless distance   yplus :  0.43091E+03 0.95307E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63138E+01      64   0.13912E-02   0.20703E-01 
c  VelocityX    0.46299E+04      12   0.65276E-02   0.40686E-03 
c  VelocityY    0.46299E+04      12   0.65276E-02   0.35942E-04 
c  VelocityZ    0.46299E+04      12   0.65276E-02   0.58194E-04 
c  TurbEner     0.59771E+01      13   0.70252E-04   0.84345E-09 
c  Dissip       0.14845E+01      14   0.65440E-03   0.54597E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.3           54509           26777           27271
v  Velocity[x]            0.29242          2.1448         0.90805         0.90983
v  Velocity[y]           -0.38284         0.69678      0.00054265      0.00032048
v  Velocity[z]           -0.42176         0.51055      -0.0012532      -0.0013769
v  TurbEner             0.0010183        0.014746        0.003287       0.0033464
v  Dissip              9.1992e-05        0.030851      0.00045242        0.000391
v  TurbVisc               0.16646           11.32          4.7137          5.2749
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              792:        0.91002E-01

===============================================================


 INSTANT    0.793000000E+03   TIME STEP NUMBER             793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999654E+04
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 :  0.23779E+00 0.12165E+01
   Friction velocity        uet   :  0.14224E-01 0.72513E-01
   Friction velocity        uk    :  0.17478E-01 0.38771E-01
   Dimensionless distance   yplus :  0.42995E+03 0.95306E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58195E+01      60   0.13355E-02   0.19065E-01 
c  VelocityX    0.46300E+04      12   0.72173E-02   0.35896E-03 
c  VelocityY    0.46300E+04      12   0.72173E-02   0.24249E-04 
c  VelocityZ    0.46300E+04      12   0.72173E-02   0.30708E-04 
c  TurbEner     0.59779E+01      13   0.75451E-04   0.81671E-09 
c  Dissip       0.15012E+01      15   0.66342E-03   0.10386E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.28           54513           26776           27270
v  Velocity[x]             0.2927          2.1834         0.90806         0.90984
v  Velocity[y]           -0.36737         0.70653      0.00055082      0.00032709
v  Velocity[z]           -0.42156         0.50444      -0.0012499      -0.0013705
v  TurbEner              0.001019        0.014857       0.0032867       0.0033462
v  Dissip              9.2039e-05        0.031029      0.00045241      0.00039099
v  TurbVisc               0.16569          11.351          4.7136          5.2748
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              793:        0.90577E-01

===============================================================


 INSTANT    0.794000000E+03   TIME STEP NUMBER             794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002225E+04
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 :  0.23778E+00 0.13234E+01
   Friction velocity        uet   :  0.14223E-01 0.78881E-01
   Friction velocity        uk    :  0.17484E-01 0.38784E-01
   Dimensionless distance   yplus :  0.42925E+03 0.95223E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66790E+01      60   0.16355E-02   0.21909E-01 
c  VelocityX    0.46298E+04      12   0.64722E-02   0.42622E-03 
c  VelocityY    0.46298E+04      12   0.64722E-02   0.39142E-04 
c  VelocityZ    0.46298E+04      12   0.64722E-02   0.34351E-04 
c  TurbEner     0.59784E+01      13   0.11854E-03   0.14197E-08 
c  Dissip       0.15115E+01      16   0.18900E-02   0.38573E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -171.1           54491           26776           27271
v  Velocity[x]            0.29317          2.0096         0.90805         0.90983
v  Velocity[y]           -0.38221         0.69963      0.00055282      0.00033252
v  Velocity[z]           -0.41922         0.51195      -0.0012475      -0.0013682
v  TurbEner             0.0010175        0.015437       0.0032868       0.0033462
v  Dissip              9.2039e-05        0.032502      0.00045254      0.00039109
v  TurbVisc               0.16539          11.332          4.7134          5.2745
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              794:        0.90238E-01

===============================================================


 INSTANT    0.795000000E+03   TIME STEP NUMBER             795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999088E+04
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 :  0.23733E+00 0.12285E+01
   Friction velocity        uet   :  0.14198E-01 0.72557E-01
   Friction velocity        uk    :  0.17471E-01 0.38782E-01
   Dimensionless distance   yplus :  0.42937E+03 0.95138E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60354E+01      54   0.13511E-02   0.19790E-01 
c  VelocityX    0.46299E+04      12   0.62171E-02   0.30223E-03 
c  VelocityY    0.46299E+04      12   0.62171E-02   0.39895E-04 
c  VelocityZ    0.46299E+04      12   0.62171E-02   0.60846E-04 
c  TurbEner     0.59764E+01      14   0.13228E-03   0.21950E-08 
c  Dissip       0.14798E+01      16   0.21207E-02   0.67276E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.89           54505           26776           27271
v  Velocity[x]            0.29262          2.0907         0.90804         0.90981
v  Velocity[y]           -0.36615         0.70608       0.0005555      0.00033031
v  Velocity[z]           -0.41997         0.50648      -0.0012477      -0.0013704
v  TurbEner             0.0010134        0.014888       0.0032863       0.0033458
v  Dissip              9.2059e-05        0.031167      0.00045219      0.00039084
v  TurbVisc               0.16541          11.345          4.7133          5.2745
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              795:        0.89295E-01

===============================================================


 INSTANT    0.796000000E+03   TIME STEP NUMBER             796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999977E+04
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 :  0.23787E+00 0.13257E+01
   Friction velocity        uet   :  0.14231E-01 0.79014E-01
   Friction velocity        uk    :  0.17436E-01 0.38635E-01
   Dimensionless distance   yplus :  0.42885E+03 0.95043E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56671E+01      51   0.13550E-02   0.18577E-01 
c  VelocityX    0.46298E+04      12   0.73848E-02   0.30939E-03 
c  VelocityY    0.46298E+04      12   0.73848E-02   0.24220E-04 
c  VelocityZ    0.46298E+04      12   0.73848E-02   0.39524E-04 
c  TurbEner     0.59765E+01      12   0.60420E-04   0.55297E-09 
c  Dissip       0.14814E+01      14   0.60218E-03   0.46317E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.85           54514           26777           27271
v  Velocity[x]            0.29258          2.1417         0.90805         0.90983
v  Velocity[y]           -0.38223         0.69967       0.0005463      0.00032459
v  Velocity[z]           -0.42085         0.51118      -0.0012494      -0.0013734
v  TurbEner              0.001013        0.014758       0.0032861       0.0033456
v  Dissip              9.2084e-05        0.030793      0.00045207      0.00039075
v  TurbVisc               0.16488          11.312           4.713          5.2742
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              796:        0.88941E-01

===============================================================


 INSTANT    0.797000000E+03   TIME STEP NUMBER             797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998582E+04
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 :  0.23800E+00 0.12443E+01
   Friction velocity        uet   :  0.14240E-01 0.72697E-01
   Friction velocity        uk    :  0.17433E-01 0.38694E-01
   Dimensionless distance   yplus :  0.42792E+03 0.94926E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62636E+01      56   0.14513E-02   0.20530E-01 
c  VelocityX    0.46299E+04      12   0.74348E-02   0.36381E-03 
c  VelocityY    0.46299E+04      12   0.74348E-02   0.37135E-04 
c  VelocityZ    0.46299E+04      12   0.74348E-02   0.86015E-04 
c  TurbEner     0.59773E+01      13   0.75758E-04   0.90651E-09 
c  Dissip       0.14986E+01      15   0.62968E-03   0.98657E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.69           54515           26776           27270
v  Velocity[x]            0.29289          2.1847         0.90805         0.90982
v  Velocity[y]            -0.3677         0.70855      0.00055861      0.00033599
v  Velocity[z]           -0.42169          0.5042      -0.0012301      -0.0013542
v  TurbEner             0.0010138        0.014824       0.0032861       0.0033456
v  Dissip              9.2087e-05        0.030903      0.00045215      0.00039081
v  TurbVisc               0.16449           11.31          4.7129          5.2741
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              797:        0.89795E-01

===============================================================


 INSTANT    0.798000000E+03   TIME STEP NUMBER             798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001499E+04
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 :  0.23735E+00 0.13253E+01
   Friction velocity        uet   :  0.14202E-01 0.78992E-01
   Friction velocity        uk    :  0.17439E-01 0.38654E-01
   Dimensionless distance   yplus :  0.42862E+03 0.94815E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58876E+01      58   0.14596E-02   0.19320E-01 
c  VelocityX    0.46299E+04      12   0.68922E-02   0.39576E-03 
c  VelocityY    0.46299E+04      12   0.68922E-02   0.25339E-04 
c  VelocityZ    0.46299E+04      12   0.68922E-02   0.49535E-04 
c  TurbEner     0.59766E+01      13   0.12259E-03   0.15134E-08 
c  Dissip       0.15102E+01      16   0.19820E-02   0.42280E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.61           54506           26777           27271
v  Velocity[x]            0.29279          2.0209         0.90805         0.90983
v  Velocity[y]           -0.38248         0.69907      0.00054467      0.00032295
v  Velocity[z]           -0.42052         0.51175      -0.0012533      -0.0013777
v  TurbEner             0.0010085        0.015403       0.0032858       0.0033453
v  Dissip              9.2086e-05        0.032448      0.00045226      0.00039088
v  TurbVisc               0.16485          11.341          4.7128           5.274
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              798:        0.90206E-01

===============================================================


 INSTANT    0.799000000E+03   TIME STEP NUMBER             799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998250E+04
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 :  0.23797E+00 0.12162E+01
   Friction velocity        uet   :  0.14240E-01 0.72488E-01
   Friction velocity        uk    :  0.17394E-01 0.38661E-01
   Dimensionless distance   yplus :  0.42786E+03 0.94777E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63091E+01      54   0.15063E-02   0.20671E-01 
c  VelocityX    0.46299E+04      12   0.74538E-02   0.38353E-03 
c  VelocityY    0.46299E+04      12   0.74538E-02   0.24357E-04 
c  VelocityZ    0.46299E+04      12   0.74538E-02   0.53335E-04 
c  TurbEner     0.59751E+01      13   0.12803E-03   0.17530E-08 
c  Dissip       0.14776E+01      16   0.20939E-02   0.65943E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.66           54509           26777           27271
v  Velocity[x]            0.29291          2.0925         0.90805         0.90982
v  Velocity[y]           -0.36657         0.70628      0.00055139      0.00032832
v  Velocity[z]           -0.42192           0.506      -0.0012505      -0.0013736
v  TurbEner             0.0010101        0.014846       0.0032853       0.0033449
v  Dissip              9.2058e-05        0.031142      0.00045191      0.00039064
v  TurbVisc               0.16421           11.33          4.7126          5.2738
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              799:        0.88785E-01

===============================================================


 INSTANT    0.800000000E+03   TIME STEP NUMBER             800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999679E+04
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 :  0.23774E+00 0.13247E+01
   Friction velocity        uet   :  0.14227E-01 0.78945E-01
   Friction velocity        uk    :  0.17408E-01 0.38672E-01
   Dimensionless distance   yplus :  0.42736E+03 0.94749E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66769E+01      53   0.14645E-02   0.21889E-01 
c  VelocityX    0.46298E+04      12   0.68593E-02   0.42482E-03 
c  VelocityY    0.46298E+04      12   0.68593E-02   0.25410E-04 
c  VelocityZ    0.46298E+04      12   0.68593E-02   0.53244E-04 
c  TurbEner     0.59751E+01      12   0.67304E-04   0.75739E-09 
c  Dissip       0.14799E+01      14   0.54793E-03   0.42043E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.93           54499           26777           27271
v  Velocity[x]            0.29278          2.1398         0.90806         0.90984
v  Velocity[y]           -0.38224         0.69918      0.00055422       0.0003332
v  Velocity[z]           -0.41974         0.51103      -0.0012482      -0.0013691
v  TurbEner             0.0010099        0.014733       0.0032851       0.0033447
v  Dissip              9.2104e-05         0.03081      0.00045183      0.00039057
v  TurbVisc               0.16411          11.341          4.7124          5.2737
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              800:        0.90324E-01

===============================================================


 INSTANT    0.801000000E+03   TIME STEP NUMBER             801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999509E+04
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 :  0.23749E+00 0.12369E+01
   Friction velocity        uet   :  0.14212E-01 0.72333E-01
   Friction velocity        uk    :  0.17406E-01 0.38659E-01
   Dimensionless distance   yplus :  0.42776E+03 0.94752E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66410E+01      57   0.13875E-02   0.21769E-01 
c  VelocityX    0.46299E+04      13   0.70882E-02   0.34374E-03 
c  VelocityY    0.46299E+04      13   0.70882E-02   0.74529E-04 
c  VelocityZ    0.46299E+04      13   0.70882E-02   0.10705E-03 
c  TurbEner     0.59755E+01      13   0.73432E-04   0.10589E-08 
c  Dissip       0.14997E+01      15   0.67264E-03   0.11149E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.95           54519           26776           27270
v  Velocity[x]            0.29263          2.1828         0.90804         0.90982
v  Velocity[y]           -0.36697         0.70783      0.00055735      0.00033179
v  Velocity[z]           -0.42032         0.50476      -0.0012394      -0.0013628
v  TurbEner             0.0010069        0.014832       0.0032849       0.0033445
v  Dissip              9.2092e-05        0.030977      0.00045183      0.00039055
v  TurbVisc               0.16437          11.382          4.7124          5.2736
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              801:        0.90341E-01

===============================================================


 INSTANT    0.802000000E+03   TIME STEP NUMBER             802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002071E+04
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 :  0.23783E+00 0.13253E+01
   Friction velocity        uet   :  0.14233E-01 0.78992E-01
   Friction velocity        uk    :  0.17380E-01 0.38630E-01
   Dimensionless distance   yplus :  0.42750E+03 0.94761E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63074E+01      58   0.15041E-02   0.20696E-01 
c  VelocityX    0.46298E+04      12   0.67643E-02   0.39960E-03 
c  VelocityY    0.46298E+04      12   0.67643E-02   0.31444E-04 
c  VelocityZ    0.46298E+04      12   0.67643E-02   0.50793E-04 
c  TurbEner     0.59760E+01      13   0.12731E-03   0.16092E-08 
c  Dissip       0.15127E+01      16   0.19560E-02   0.42858E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.11           54522           26777           27271
v  Velocity[x]            0.29257          2.0161         0.90806         0.90983
v  Velocity[y]           -0.38246         0.69843      0.00054851      0.00032512
v  Velocity[z]            -0.4229         0.51174       -0.001253      -0.0013748
v  TurbEner             0.0010078        0.015433       0.0032849       0.0033445
v  Dissip              9.2072e-05        0.032484      0.00045198      0.00039065
v  TurbVisc               0.16413          11.363          4.7123          5.2735
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              802:        0.90455E-01

===============================================================


 INSTANT    0.803000000E+03   TIME STEP NUMBER             803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998186E+04
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 :  0.23774E+00 0.12602E+01
   Friction velocity        uet   :  0.14228E-01 0.73330E-01
   Friction velocity        uk    :  0.17388E-01 0.38675E-01
   Dimensionless distance   yplus :  0.42678E+03 0.94780E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60090E+01      63   0.13054E-02   0.19679E-01 
c  VelocityX    0.46298E+04      12   0.68857E-02   0.39133E-03 
c  VelocityY    0.46298E+04      12   0.68857E-02   0.27385E-04 
c  VelocityZ    0.46298E+04      12   0.68857E-02   0.51766E-04 
c  TurbEner     0.59744E+01      13   0.13405E-03   0.18268E-08 
c  Dissip       0.14743E+01      17   0.22915E-02   0.76322E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.16           54534           26776           27270
v  Velocity[x]            0.29323          2.0927         0.90804         0.90982
v  Velocity[y]           -0.36692         0.70561       0.0005525      0.00032626
v  Velocity[z]           -0.41944         0.50563      -0.0012459      -0.0013665
v  TurbEner             0.0010099        0.014855       0.0032846       0.0033442
v  Dissip              9.2053e-05        0.031025      0.00045165      0.00039041
v  TurbVisc               0.16392          11.364          4.7123          5.2735
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              803:        0.90986E-01

===============================================================


 INSTANT    0.804000000E+03   TIME STEP NUMBER             804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002112E+04
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 :  0.23768E+00 0.13245E+01
   Friction velocity        uet   :  0.14225E-01 0.78936E-01
   Friction velocity        uk    :  0.17406E-01 0.38604E-01
   Dimensionless distance   yplus :  0.42762E+03 0.94801E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57092E+01      54   0.12274E-02   0.18725E-01 
c  VelocityX    0.46299E+04      12   0.64689E-02   0.32047E-03 
c  VelocityY    0.46299E+04      12   0.64689E-02   0.23417E-04 
c  VelocityZ    0.46299E+04      12   0.64689E-02   0.53829E-04 
c  TurbEner     0.59749E+01      12   0.65691E-04   0.60287E-09 
c  Dissip       0.14760E+01      14   0.54205E-03   0.38695E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.91           54544           26777           27271
v  Velocity[x]            0.29262          2.1407         0.90806         0.90984
v  Velocity[y]           -0.38281          0.6992      0.00054083      0.00031917
v  Velocity[z]           -0.42089         0.51052      -0.0012571      -0.0013791
v  TurbEner             0.0010068        0.014767       0.0032846       0.0033442
v  Dissip              9.2078e-05        0.030689      0.00045158      0.00039036
v  TurbVisc               0.16449          11.335          4.7121          5.2734
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              804:        0.89624E-01

===============================================================


 INSTANT    0.805000000E+03   TIME STEP NUMBER             805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998171E+04
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 :  0.23775E+00 0.12133E+01
   Friction velocity        uet   :  0.14230E-01 0.72313E-01
   Friction velocity        uk    :  0.17380E-01 0.38641E-01
   Dimensionless distance   yplus :  0.42723E+03 0.94819E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62585E+01      55   0.14375E-02   0.20509E-01 
c  VelocityX    0.46299E+04      13   0.73872E-02   0.29158E-03 
c  VelocityY    0.46299E+04      13   0.73872E-02   0.63109E-04 
c  VelocityZ    0.46299E+04      13   0.73872E-02   0.10700E-03 
c  TurbEner     0.59761E+01      13   0.75999E-04   0.93111E-09 
c  Dissip       0.14971E+01      15   0.69486E-03   0.11564E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.46           54537           26776           27270
v  Velocity[x]             0.2924          2.1827         0.90805         0.90982
v  Velocity[y]           -0.36736         0.70771      0.00055975      0.00033496
v  Velocity[z]           -0.42236          0.5043      -0.0012361       -0.001359
v  TurbEner             0.0010108        0.014893       0.0032845       0.0033442
v  Dissip              9.2043e-05        0.030903      0.00045165       0.0003904
v  TurbVisc               0.16428          11.325          4.7122          5.2735
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              805:        0.89807E-01

===============================================================


 INSTANT    0.806000000E+03   TIME STEP NUMBER             806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000825E+04
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 :  0.23778E+00 0.13253E+01
   Friction velocity        uet   :  0.14232E-01 0.78995E-01
   Friction velocity        uk    :  0.17414E-01 0.38691E-01
   Dimensionless distance   yplus :  0.42727E+03 0.94824E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61462E+01      68   0.16587E-02   0.20157E-01 
c  VelocityX    0.46298E+04      12   0.66333E-02   0.39177E-03 
c  VelocityY    0.46298E+04      12   0.66333E-02   0.26178E-04 
c  VelocityZ    0.46298E+04      12   0.66333E-02   0.50815E-04 
c  TurbEner     0.59767E+01      13   0.13120E-03   0.17697E-08 
c  Dissip       0.15115E+01      16   0.19979E-02   0.45936E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.17           54515           26777           27271
v  Velocity[x]            0.29303          2.0173         0.90806         0.90984
v  Velocity[y]           -0.38226         0.69768      0.00055287      0.00033281
v  Velocity[z]           -0.42088         0.51193      -0.0012357      -0.0013565
v  TurbEner             0.0010127        0.015509       0.0032847       0.0033443
v  Dissip              9.2054e-05        0.032447      0.00045191       0.0003906
v  TurbVisc               0.16441          11.355          4.7122          5.2735
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              806:        0.91952E-01

===============================================================


 INSTANT    0.807000000E+03   TIME STEP NUMBER             807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998776E+04
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 :  0.23770E+00 0.12419E+01
   Friction velocity        uet   :  0.14227E-01 0.72581E-01
   Friction velocity        uk    :  0.17430E-01 0.38726E-01
   Dimensionless distance   yplus :  0.42809E+03 0.94837E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58222E+01      53   0.13019E-02   0.19094E-01 
c  VelocityX    0.46299E+04      12   0.66831E-02   0.33591E-03 
c  VelocityY    0.46299E+04      12   0.66831E-02   0.26743E-04 
c  VelocityZ    0.46299E+04      12   0.66831E-02   0.49205E-04 
c  TurbEner     0.59749E+01      14   0.13189E-03   0.20382E-08 
c  Dissip       0.14747E+01      16   0.22102E-02   0.73028E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.29           54521           26777           27271
v  Velocity[x]            0.29281          2.0916         0.90805         0.90983
v  Velocity[y]           -0.36606         0.70587      0.00054942      0.00032497
v  Velocity[z]           -0.42204         0.50654      -0.0012445      -0.0013662
v  TurbEner             0.0010113        0.014939       0.0032846       0.0033443
v  Dissip               9.204e-05        0.031046      0.00045168      0.00039044
v  TurbVisc               0.16489          11.404          4.7122          5.2735
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              807:        0.89039E-01

===============================================================


 INSTANT    0.808000000E+03   TIME STEP NUMBER             808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000861E+04
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 :  0.23768E+00 0.13241E+01
   Friction velocity        uet   :  0.14226E-01 0.78918E-01
   Friction velocity        uk    :  0.17418E-01 0.38752E-01
   Dimensionless distance   yplus :  0.42818E+03 0.94860E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65324E+01      55   0.13281E-02   0.21407E-01 
c  VelocityX    0.46299E+04      12   0.68193E-02   0.40119E-03 
c  VelocityY    0.46299E+04      12   0.68193E-02   0.26155E-04 
c  VelocityZ    0.46299E+04      12   0.68193E-02   0.50512E-04 
c  TurbEner     0.59752E+01      13   0.68549E-04   0.71367E-09 
c  Dissip       0.14770E+01      14   0.54127E-03   0.37684E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.29           54535           26777           27271
v  Velocity[x]            0.29258          2.1422         0.90807         0.90984
v  Velocity[y]           -0.38221         0.70108      0.00054495      0.00032519
v  Velocity[z]           -0.42275         0.51107      -0.0012507      -0.0013716
v  TurbEner             0.0010133        0.014824       0.0032845       0.0033442
v  Dissip              9.2125e-05        0.030698      0.00045164      0.00039041
v  TurbVisc               0.16485          11.389          4.7123          5.2736
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              808:        0.88985E-01

===============================================================


 INSTANT    0.809000000E+03   TIME STEP NUMBER             809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998978E+04
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 :  0.23770E+00 0.12140E+01
   Friction velocity        uet   :  0.14228E-01 0.72358E-01
   Friction velocity        uk    :  0.17435E-01 0.38740E-01
   Dimensionless distance   yplus :  0.42772E+03 0.94895E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75335E+01      60   0.14680E-02   0.24691E-01 
c  VelocityX    0.46299E+04      13   0.74060E-02   0.37803E-03 
c  VelocityY    0.46299E+04      13   0.74060E-02   0.56239E-04 
c  VelocityZ    0.46299E+04      13   0.74060E-02   0.99248E-04 
c  TurbEner     0.59762E+01      12   0.71843E-04   0.72052E-09 
c  Dissip       0.14982E+01      15   0.67713E-03   0.11338E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.24           54540           26776           27270
v  Velocity[x]            0.29294          2.1885         0.90803         0.90981
v  Velocity[y]           -0.36772         0.71035      0.00056591       0.0003392
v  Velocity[z]           -0.42014         0.50419      -0.0012354       -0.001358
v  TurbEner              0.001016        0.014906       0.0032846       0.0033442
v  Dissip              9.2213e-05        0.030826      0.00045173      0.00039046
v  TurbVisc               0.16464          11.392          4.7123          5.2736
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              809:        0.90587E-01

===============================================================


 INSTANT    0.810000000E+03   TIME STEP NUMBER             810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001842E+04
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 :  0.23732E+00 0.13252E+01
   Friction velocity        uet   :  0.14205E-01 0.78982E-01
   Friction velocity        uk    :  0.17459E-01 0.38647E-01
   Dimensionless distance   yplus :  0.42883E+03 0.94857E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67429E+01      68   0.14895E-02   0.22131E-01 
c  VelocityX    0.46298E+04      12   0.67309E-02   0.37603E-03 
c  VelocityY    0.46298E+04      12   0.67309E-02   0.38691E-04 
c  VelocityZ    0.46298E+04      12   0.67309E-02   0.53101E-04 
c  TurbEner     0.59764E+01      13   0.13766E-03   0.16327E-08 
c  Dissip       0.15035E+01      16   0.19159E-02   0.40096E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.15           54551           26777           27272
v  Velocity[x]            0.29258          2.0063         0.90804         0.90983
v  Velocity[y]           -0.38252         0.69759      0.00055337      0.00032758
v  Velocity[z]           -0.42036         0.51167      -0.0012472      -0.0013717
v  TurbEner             0.0010126        0.015578       0.0032846       0.0033442
v  Dissip              9.2226e-05        0.032325      0.00045185      0.00039054
v  TurbVisc               0.16523          11.362          4.7124          5.2737
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              810:        0.91021E-01

===============================================================


 INSTANT    0.811000000E+03   TIME STEP NUMBER             811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997515E+04
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 :  0.23785E+00 0.12286E+01
   Friction velocity        uet   :  0.14237E-01 0.72665E-01
   Friction velocity        uk    :  0.17429E-01 0.38525E-01
   Dimensionless distance   yplus :  0.42842E+03 0.94862E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66054E+01      56   0.15121E-02   0.21643E-01 
c  VelocityX    0.46299E+04      12   0.75047E-02   0.39648E-03 
c  VelocityY    0.46299E+04      12   0.75047E-02   0.22933E-04 
c  VelocityZ    0.46299E+04      12   0.75047E-02   0.35239E-04 
c  TurbEner     0.59753E+01      14   0.14596E-03   0.20152E-08 
c  Dissip       0.14639E+01      17   0.24639E-02   0.80827E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.04           54542           26777           27271
v  Velocity[x]            0.29284           2.098         0.90806         0.90983
v  Velocity[y]           -0.36669          0.7071      0.00055033      0.00032773
v  Velocity[z]           -0.42122         0.50591      -0.0012489      -0.0013716
v  TurbEner             0.0010153        0.014869       0.0032845       0.0033441
v  Dissip              9.2141e-05        0.030642      0.00045153      0.00039032
v  TurbVisc               0.16489          11.358          4.7124          5.2737
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              811:        0.89753E-01

===============================================================


 INSTANT    0.812000000E+03   TIME STEP NUMBER             812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001988E+04
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 :  0.23791E+00 0.13233E+01
   Friction velocity        uet   :  0.14240E-01 0.78855E-01
   Friction velocity        uk    :  0.17452E-01 0.38648E-01
   Dimensionless distance   yplus :  0.42821E+03 0.94794E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70365E+01      61   0.14666E-02   0.23055E-01 
c  VelocityX    0.46299E+04      12   0.76084E-02   0.44639E-03 
c  VelocityY    0.46299E+04      12   0.76084E-02   0.30591E-04 
c  VelocityZ    0.46299E+04      12   0.76084E-02   0.51948E-04 
c  TurbEner     0.59760E+01      13   0.79546E-04   0.11429E-08 
c  Dissip       0.14672E+01      14   0.33973E-03   0.24107E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.38           54515           26776           27271
v  Velocity[x]            0.29299          2.1403         0.90808         0.90986
v  Velocity[y]           -0.38233         0.69995      0.00054749      0.00032719
v  Velocity[z]           -0.42139         0.51105      -0.0012484      -0.0013692
v  TurbEner             0.0010153        0.014808       0.0032847       0.0033443
v  Dissip              9.2133e-05        0.030453      0.00045153      0.00039032
v  TurbVisc                0.1648          11.324          4.7124          5.2737
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              812:        0.90560E-01

===============================================================


 INSTANT    0.813000000E+03   TIME STEP NUMBER             813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000919E+04
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 :  0.23759E+00 0.12194E+01
   Friction velocity        uet   :  0.14220E-01 0.72532E-01
   Friction velocity        uk    :  0.17452E-01 0.38720E-01
   Dimensionless distance   yplus :  0.42866E+03 0.94676E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65544E+01      58   0.13423E-02   0.21494E-01 
c  VelocityX    0.46300E+04      13   0.65596E-02   0.41658E-03 
c  VelocityY    0.46300E+04      13   0.65596E-02   0.41555E-04 
c  VelocityZ    0.46300E+04      13   0.65596E-02   0.11998E-03 
c  TurbEner     0.59764E+01      13   0.73664E-04   0.12562E-08 
c  Dissip       0.14895E+01      15   0.68347E-03   0.11008E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.88           54531           26776           27270
v  Velocity[x]            0.29257          2.1771         0.90805         0.90982
v  Velocity[y]           -0.36698         0.70742      0.00056459      0.00033812
v  Velocity[z]           -0.42221         0.50472      -0.0012518      -0.0013699
v  TurbEner             0.0010125        0.014968       0.0032848       0.0033444
v  Dissip              9.2073e-05        0.030745      0.00045164      0.00039039
v  TurbVisc               0.16504          11.318          4.7125          5.2739
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              813:        0.90566E-01

===============================================================


 INSTANT    0.814000000E+03   TIME STEP NUMBER             814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001709E+04
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 :  0.23767E+00 0.13239E+01
   Friction velocity        uet   :  0.14224E-01 0.78892E-01
   Friction velocity        uk    :  0.17428E-01 0.38697E-01
   Dimensionless distance   yplus :  0.42852E+03 0.94597E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65820E+01      57   0.13730E-02   0.21580E-01 
c  VelocityX    0.46299E+04      12   0.70134E-02   0.32022E-03 
c  VelocityY    0.46299E+04      12   0.70134E-02   0.55234E-04 
c  VelocityZ    0.46299E+04      12   0.70134E-02   0.59572E-04 
c  TurbEner     0.59772E+01      13   0.84469E-04   0.13886E-08 
c  Dissip       0.15091E+01      15   0.90792E-03   0.18763E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.01           54533           26776           27271
v  Velocity[x]            0.29276           2.192         0.90807         0.90985
v  Velocity[y]           -0.38237          0.6997      0.00054844      0.00032484
v  Velocity[z]            -0.4219         0.51188      -0.0012557      -0.0013737
v  TurbEner             0.0010132        0.015171        0.003285       0.0033445
v  Dissip              9.2057e-05        0.031172      0.00045182       0.0003905
v  TurbVisc               0.16485           11.36          4.7126          5.2739
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              814:        0.89754E-01

===============================================================


 INSTANT    0.815000000E+03   TIME STEP NUMBER             815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999021E+04
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 :  0.23786E+00 0.12350E+01
   Friction velocity        uet   :  0.14235E-01 0.72521E-01
   Friction velocity        uk    :  0.17434E-01 0.38651E-01
   Dimensionless distance   yplus :  0.42791E+03 0.94493E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72342E+01      58   0.16327E-02   0.23712E-01 
c  VelocityX    0.46299E+04      12   0.70390E-02   0.38325E-03 
c  VelocityY    0.46299E+04      12   0.70390E-02   0.42517E-04 
c  VelocityZ    0.46299E+04      12   0.70390E-02   0.28744E-04 
c  TurbEner     0.59783E+01      13   0.12535E-03   0.14431E-08 
c  Dissip       0.15298E+01      16   0.21646E-02   0.52940E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.41           54541           26776           27270
v  Velocity[x]            0.29281          2.0393         0.90805         0.90982
v  Velocity[y]           -0.36691         0.70832      0.00055618      0.00033138
v  Velocity[z]           -0.41983         0.50573      -0.0012585      -0.0013777
v  TurbEner             0.0010146        0.015775       0.0032853       0.0033447
v  Dissip              9.2013e-05        0.032905      0.00045213      0.00039072
v  TurbVisc               0.16459          11.346          4.7126          5.2739
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              815:        0.89888E-01

===============================================================


 INSTANT    0.816000000E+03   TIME STEP NUMBER             816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001594E+04
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 :  0.23739E+00 0.13241E+01
   Friction velocity        uet   :  0.14205E-01 0.78909E-01
   Friction velocity        uk    :  0.17447E-01 0.38558E-01
   Dimensionless distance   yplus :  0.42881E+03 0.94516E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65567E+01      58   0.13081E-02   0.21498E-01 
c  VelocityX    0.46299E+04      12   0.68225E-02   0.37072E-03 
c  VelocityY    0.46299E+04      12   0.68225E-02   0.35437E-04 
c  VelocityZ    0.46299E+04      12   0.68225E-02   0.42033E-04 
c  TurbEner     0.59774E+01      13   0.12870E-03   0.16643E-08 
c  Dissip       0.15031E+01      16   0.18167E-02   0.48748E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.48           54551           26777           27271
v  Velocity[x]            0.29281          2.1011         0.90806         0.90984
v  Velocity[y]            -0.3828         0.70045      0.00053298       0.0003116
v  Velocity[z]           -0.42017          0.5105       -0.001253       -0.001376
v  TurbEner             0.0010098        0.015203       0.0032854       0.0033448
v  Dissip              9.2023e-05        0.031677      0.00045203      0.00039066
v  TurbVisc               0.16512          11.354          4.7127           5.274
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              816:        0.90077E-01

===============================================================


 INSTANT    0.817000000E+03   TIME STEP NUMBER             817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997510E+04
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 :  0.23788E+00 0.12344E+01
   Friction velocity        uet   :  0.14234E-01 0.72534E-01
   Friction velocity        uk    :  0.17405E-01 0.38575E-01
   Dimensionless distance   yplus :  0.42818E+03 0.94517E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57801E+01      53   0.15552E-02   0.18952E-01 
c  VelocityX    0.46299E+04      12   0.71603E-02   0.33046E-03 
c  VelocityY    0.46299E+04      12   0.71603E-02   0.27446E-04 
c  VelocityZ    0.46299E+04      12   0.71603E-02   0.57732E-04 
c  TurbEner     0.59781E+01      12   0.58584E-04   0.66606E-09 
c  Dissip       0.15114E+01      13   0.18894E-03   0.11813E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.59           54541           26777           27271
v  Velocity[x]            0.29282          2.1506         0.90806         0.90984
v  Velocity[y]           -0.36738         0.70763      0.00054754      0.00032318
v  Velocity[z]           -0.42138         0.50438      -0.0012494      -0.0013702
v  TurbEner             0.0010118         0.01516       0.0032856        0.003345
v  Dissip                 9.2e-05        0.031676      0.00045209      0.00039071
v  TurbVisc               0.16467          11.332          4.7127           5.274
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              817:        0.88797E-01

===============================================================


 INSTANT    0.818000000E+03   TIME STEP NUMBER             818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999744E+04
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 :  0.23780E+00 0.13250E+01
   Friction velocity        uet   :  0.14227E-01 0.78956E-01
   Friction velocity        uk    :  0.17423E-01 0.38644E-01
   Dimensionless distance   yplus :  0.42780E+03 0.94454E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63466E+01      55   0.15416E-02   0.20805E-01 
c  VelocityX    0.46299E+04      12   0.73564E-02   0.38721E-03 
c  VelocityY    0.46299E+04      12   0.73564E-02   0.27019E-04 
c  VelocityZ    0.46299E+04      12   0.73564E-02   0.46672E-04 
c  TurbEner     0.59792E+01      13   0.71269E-04   0.11596E-08 
c  Dissip       0.15337E+01      15   0.77530E-03   0.16055E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.57           54517           26777           27272
v  Velocity[x]            0.29272          2.1854         0.90808         0.90986
v  Velocity[y]           -0.38227         0.70045       0.0005567       0.0003348
v  Velocity[z]           -0.42196         0.51188      -0.0012384      -0.0013601
v  TurbEner              0.001012        0.015201       0.0032858       0.0033452
v  Dissip              9.2035e-05        0.031841      0.00045236       0.0003909
v  TurbVisc               0.16465          11.327          4.7128          5.2741
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              818:        0.89602E-01

===============================================================


 INSTANT    0.819000000E+03   TIME STEP NUMBER             819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998982E+04
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 :  0.23742E+00 0.12139E+01
   Friction velocity        uet   :  0.14203E-01 0.72343E-01
   Friction velocity        uk    :  0.17425E-01 0.38646E-01
   Dimensionless distance   yplus :  0.42828E+03 0.94431E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61249E+01      54   0.14953E-02   0.20093E-01 
c  VelocityX    0.46300E+04      12   0.72751E-02   0.34906E-03 
c  VelocityY    0.46300E+04      12   0.72751E-02   0.27649E-04 
c  VelocityZ    0.46300E+04      12   0.72751E-02   0.36522E-04 
c  TurbEner     0.59788E+01      13   0.10622E-03   0.13226E-08 
c  Dissip       0.15456E+01      16   0.18380E-02   0.39703E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.3           54523           26777           27271
v  Velocity[x]            0.29255          2.0299         0.90805         0.90982
v  Velocity[y]           -0.36615         0.70882      0.00054692      0.00032284
v  Velocity[z]           -0.42081         0.50645      -0.0012608      -0.0013815
v  TurbEner             0.0010097        0.015695        0.003286       0.0033454
v  Dissip              9.2044e-05         0.03329      0.00045259      0.00039106
v  TurbVisc               0.16501          11.354          4.7128          5.2741
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              819:        0.89392E-01

===============================================================


 INSTANT    0.820000000E+03   TIME STEP NUMBER             820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001184E+04
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 :  0.23802E+00 0.13247E+01
   Friction velocity        uet   :  0.14239E-01 0.78955E-01
   Friction velocity        uk    :  0.17404E-01 0.38515E-01
   Dimensionless distance   yplus :  0.42811E+03 0.94412E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66112E+01      54   0.13310E-02   0.21674E-01 
c  VelocityX    0.46299E+04      12   0.67618E-02   0.37052E-03 
c  VelocityY    0.46299E+04      12   0.67618E-02   0.34523E-04 
c  VelocityZ    0.46299E+04      12   0.67618E-02   0.10377E-03 
c  TurbEner     0.59774E+01      13   0.13707E-03   0.19706E-08 
c  Dissip       0.15091E+01      16   0.22515E-02   0.75633E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -165.72           54534           26777           27271
v  Velocity[x]            0.29274          2.0977         0.90806         0.90984
v  Velocity[y]           -0.38226         0.69663      0.00054928       0.0003272
v  Velocity[z]           -0.42216         0.51109      -0.0012554      -0.0013763
v  TurbEner             0.0010111        0.015102       0.0032859       0.0033453
v  Dissip              9.2056e-05        0.031827      0.00045239      0.00039093
v  TurbVisc               0.16492          11.335          4.7128          5.2741
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              820:        0.89322E-01

===============================================================


 INSTANT    0.821000000E+03   TIME STEP NUMBER             821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999168E+04
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 :  0.23770E+00 0.12418E+01
   Friction velocity        uet   :  0.14218E-01 0.72575E-01
   Friction velocity        uk    :  0.17416E-01 0.38535E-01
   Dimensionless distance   yplus :  0.42749E+03 0.94406E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61166E+01      57   0.12131E-02   0.20043E-01 
c  VelocityX    0.46299E+04      12   0.70681E-02   0.35897E-03 
c  VelocityY    0.46299E+04      12   0.70681E-02   0.27171E-04 
c  VelocityZ    0.46299E+04      12   0.70681E-02   0.31951E-04 
c  TurbEner     0.59781E+01      12   0.62811E-04   0.86651E-09 
c  Dissip       0.15185E+01      13   0.33683E-03   0.27147E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.65           54541           26776           27270
v  Velocity[x]            0.29302          2.1572         0.90804         0.90981
v  Velocity[y]           -0.36763         0.70622      0.00055136      0.00032515
v  Velocity[z]           -0.41992          0.5042      -0.0012522      -0.0013735
v  TurbEner             0.0010139        0.015011       0.0032861       0.0033454
v  Dissip              9.2053e-05        0.031728      0.00045247      0.00039099
v  TurbVisc               0.16472          11.345          4.7127           5.274
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              821:        0.89610E-01

===============================================================


 INSTANT    0.822000000E+03   TIME STEP NUMBER             822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002214E+04
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 :  0.23755E+00 0.13237E+01
   Friction velocity        uet   :  0.14208E-01 0.78896E-01
   Friction velocity        uk    :  0.17440E-01 0.38492E-01
   Dimensionless distance   yplus :  0.42855E+03 0.94481E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58270E+01      53   0.12787E-02   0.19113E-01 
c  VelocityX    0.46299E+04      12   0.70696E-02   0.35941E-03 
c  VelocityY    0.46299E+04      12   0.70696E-02   0.29191E-04 
c  VelocityZ    0.46299E+04      12   0.70696E-02   0.40548E-04 
c  TurbEner     0.59791E+01      13   0.71952E-04   0.93639E-09 
c  Dissip       0.15418E+01      15   0.83833E-03   0.16623E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.31           54549           26776           27271
v  Velocity[x]             0.2925          2.1858         0.90807         0.90985
v  Velocity[y]           -0.38246         0.70205      0.00054109      0.00031707
v  Velocity[z]           -0.42042         0.51174      -0.0012525       -0.001374
v  TurbEner             0.0010104        0.015096       0.0032864       0.0033456
v  Dissip              9.2039e-05        0.032031      0.00045271      0.00039116
v  TurbVisc               0.16537          11.328          4.7128          5.2741
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              822:        0.89290E-01

===============================================================


 INSTANT    0.823000000E+03   TIME STEP NUMBER             823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999368E+04
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 :  0.23794E+00 0.12178E+01
   Friction velocity        uet   :  0.14231E-01 0.72588E-01
   Friction velocity        uk    :  0.17411E-01 0.38565E-01
   Dimensionless distance   yplus :  0.42814E+03 0.94465E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65852E+01      57   0.16961E-02   0.21585E-01 
c  VelocityX    0.46300E+04      12   0.72589E-02   0.40477E-03 
c  VelocityY    0.46300E+04      12   0.72589E-02   0.24107E-04 
c  VelocityZ    0.46300E+04      12   0.72589E-02   0.33417E-04 
c  TurbEner     0.59794E+01      13   0.10723E-03   0.10826E-08 
c  Dissip       0.15554E+01      16   0.18909E-02   0.41419E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.23           54540           26776           27270
v  Velocity[x]            0.29273          2.0276         0.90806         0.90984
v  Velocity[y]           -0.36659          0.7097      0.00055028      0.00032798
v  Velocity[z]           -0.42283         0.50599      -0.0012613      -0.0013814
v  TurbEner             0.0010137        0.015585       0.0032865       0.0033457
v  Dissip              9.2018e-05         0.03351      0.00045291       0.0003913
v  TurbVisc               0.16509          11.326          4.7128          5.2741
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              823:        0.89668E-01

===============================================================


 INSTANT    0.824000000E+03   TIME STEP NUMBER             824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001499E+04
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 :  0.23762E+00 0.13243E+01
   Friction velocity        uet   :  0.14211E-01 0.78942E-01
   Friction velocity        uk    :  0.17439E-01 0.38603E-01
   Dimensionless distance   yplus :  0.42796E+03 0.94445E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71906E+01      66   0.16498E-02   0.23581E-01 
c  VelocityX    0.46298E+04      12   0.62468E-02   0.38626E-03 
c  VelocityY    0.46298E+04      12   0.62468E-02   0.40584E-04 
c  VelocityZ    0.46298E+04      12   0.62468E-02   0.40072E-04 
c  TurbEner     0.59781E+01      13   0.14805E-03   0.22545E-08 
c  Dissip       0.15175E+01      16   0.23226E-02   0.78283E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.99           54516           26776           27271
v  Velocity[x]            0.29276           2.089         0.90805         0.90984
v  Velocity[y]           -0.38228         0.70088      0.00055475      0.00033596
v  Velocity[z]           -0.42028           0.511      -0.0012396      -0.0013609
v  TurbEner             0.0010146        0.014968       0.0032864       0.0033457
v  Dissip              9.1998e-05        0.031995      0.00045271      0.00039118
v  TurbVisc               0.16507          11.359          4.7128           5.274
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              824:        0.91912E-01

===============================================================


 INSTANT    0.825000000E+03   TIME STEP NUMBER             825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999085E+04
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 :  0.23786E+00 0.12181E+01
   Friction velocity        uet   :  0.14225E-01 0.72605E-01
   Friction velocity        uk    :  0.17447E-01 0.38600E-01
   Dimensionless distance   yplus :  0.42856E+03 0.94441E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56241E+01      52   0.11901E-02   0.18448E-01 
c  VelocityX    0.46300E+04      12   0.65009E-02   0.29355E-03 
c  VelocityY    0.46300E+04      12   0.65009E-02   0.22576E-04 
c  VelocityZ    0.46300E+04      12   0.65009E-02   0.31175E-04 
c  TurbEner     0.59773E+01      13   0.80784E-04   0.11784E-08 
c  Dissip       0.15209E+01      14   0.46733E-03   0.35133E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.42           54523           26776           27270
v  Velocity[x]            0.29273          2.1532         0.90804         0.90982
v  Velocity[y]           -0.36696         0.70773      0.00054539      0.00032226
v  Velocity[z]           -0.42147         0.50478      -0.0012493      -0.0013709
v  TurbEner              0.001013        0.014831       0.0032862       0.0033455
v  Dissip              9.1994e-05        0.031715      0.00045267      0.00039115
v  TurbVisc               0.16542          11.339          4.7126          5.2739
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              825:        0.88728E-01

===============================================================


 INSTANT    0.826000000E+03   TIME STEP NUMBER             826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001538E+04
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 :  0.23782E+00 0.13257E+01
   Friction velocity        uet   :  0.14222E-01 0.79009E-01
   Friction velocity        uk    :  0.17432E-01 0.38579E-01
   Dimensionless distance   yplus :  0.42860E+03 0.94408E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65490E+01      55   0.13206E-02   0.21466E-01 
c  VelocityX    0.46299E+04      12   0.71603E-02   0.31325E-03 
c  VelocityY    0.46299E+04      12   0.71603E-02   0.29521E-04 
c  VelocityZ    0.46299E+04      12   0.71603E-02   0.80264E-04 
c  TurbEner     0.59775E+01      13   0.68097E-04   0.74629E-09 
c  Dissip       0.15413E+01      15   0.64070E-03   0.10012E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.65           54533           26777           27271
v  Velocity[x]            0.29287          2.1833         0.90804         0.90982
v  Velocity[y]           -0.38245         0.70073      0.00055426      0.00033236
v  Velocity[z]           -0.42219         0.51177      -0.0012461      -0.0013701
v  TurbEner             0.0010148        0.014924       0.0032861       0.0033454
v  Dissip              9.1983e-05        0.031906      0.00045275       0.0003912
v  TurbVisc               0.16537          11.342          4.7124          5.2737
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              826:        0.89209E-01

===============================================================


 INSTANT    0.827000000E+03   TIME STEP NUMBER             827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998669E+04
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 :  0.23769E+00 0.12358E+01
   Friction velocity        uet   :  0.14214E-01 0.72373E-01
   Friction velocity        uk    :  0.17448E-01 0.38589E-01
   Dimensionless distance   yplus :  0.42819E+03 0.94395E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62892E+01      58   0.12599E-02   0.20610E-01 
c  VelocityX    0.46298E+04      12   0.64441E-02   0.39724E-03 
c  VelocityY    0.46298E+04      12   0.64441E-02   0.39867E-04 
c  VelocityZ    0.46298E+04      12   0.64441E-02   0.59489E-04 
c  TurbEner     0.59776E+01      13   0.12144E-03   0.10816E-08 
c  Dissip       0.15510E+01      16   0.20340E-02   0.43940E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -176.3           54540           26775           27269
v  Velocity[x]            0.29308          2.0158         0.90805         0.90982
v  Velocity[y]           -0.36689         0.70824      0.00054948      0.00032444
v  Velocity[z]           -0.41955         0.50566      -0.0012517      -0.0013734
v  TurbEner             0.0010177        0.015523       0.0032861       0.0033454
v  Dissip              9.2028e-05        0.033509      0.00045296      0.00039136
v  TurbVisc               0.16518          11.303          4.7122          5.2735
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              827:        0.90141E-01

===============================================================


 INSTANT    0.828000000E+03   TIME STEP NUMBER             828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001862E+04
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 :  0.23742E+00 0.13259E+01
   Friction velocity        uet   :  0.14198E-01 0.79024E-01
   Friction velocity        uk    :  0.17473E-01 0.38395E-01
   Dimensionless distance   yplus :  0.42931E+03 0.94367E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54229E+01      55   0.11376E-02   0.17787E-01 
c  VelocityX    0.46299E+04      12   0.62810E-02   0.28833E-03 
c  VelocityY    0.46299E+04      12   0.62810E-02   0.33708E-04 
c  VelocityZ    0.46299E+04      12   0.62810E-02   0.33956E-04 
c  TurbEner     0.59762E+01      13   0.15800E-03   0.21114E-08 
c  Dissip       0.15074E+01      17   0.26414E-02   0.91581E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.17           54549           26776           27270
v  Velocity[x]            0.29241          2.0993         0.90807         0.90985
v  Velocity[y]           -0.38281         0.69736      0.00054116      0.00031901
v  Velocity[z]           -0.41996         0.51051      -0.0012523       -0.001374
v  TurbEner             0.0010141        0.014773       0.0032859       0.0033453
v  Dissip              9.2059e-05        0.031718      0.00045265      0.00039116
v  TurbVisc               0.16577          11.315          4.7122          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              828:        0.89774E-01

===============================================================


 INSTANT    0.829000000E+03   TIME STEP NUMBER             829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998109E+04
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 :  0.23794E+00 0.12178E+01
   Friction velocity        uet   :  0.14229E-01 0.72580E-01
   Friction velocity        uk    :  0.17442E-01 0.38478E-01
   Dimensionless distance   yplus :  0.42889E+03 0.94341E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57848E+01      56   0.14581E-02   0.18967E-01 
c  VelocityX    0.46298E+04      12   0.72533E-02   0.31079E-03 
c  VelocityY    0.46298E+04      12   0.72533E-02   0.22503E-04 
c  VelocityZ    0.46298E+04      12   0.72533E-02   0.32161E-04 
c  TurbEner     0.59766E+01      13   0.63451E-04   0.67304E-09 
c  Dissip       0.15106E+01      13   0.43089E-03   0.28216E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.31           54541           26776           27270
v  Velocity[x]             0.2926          2.1512         0.90805         0.90983
v  Velocity[y]           -0.36735         0.70569      0.00054835      0.00032569
v  Velocity[z]           -0.42093         0.50436      -0.0012534      -0.0013721
v  TurbEner             0.0010168        0.014662       0.0032859       0.0033453
v  Dissip              9.2079e-05        0.031456      0.00045257      0.00039111
v  TurbVisc               0.16541          11.339          4.7121          5.2734
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              829:        0.89250E-01

===============================================================


 INSTANT    0.830000000E+03   TIME STEP NUMBER             830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001507E+04
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 :  0.23796E+00 0.13238E+01
   Friction velocity        uet   :  0.14230E-01 0.78901E-01
   Friction velocity        uk    :  0.17465E-01 0.38522E-01
   Dimensionless distance   yplus :  0.42866E+03 0.94355E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64040E+01      63   0.15461E-02   0.20991E-01 
c  VelocityX    0.46298E+04      12   0.71296E-02   0.42532E-03 
c  VelocityY    0.46298E+04      12   0.71296E-02   0.34251E-04 
c  VelocityZ    0.46298E+04      12   0.71296E-02   0.37346E-04 
c  TurbEner     0.59768E+01      13   0.10191E-03   0.13869E-08 
c  Dissip       0.15143E+01      16   0.15538E-02   0.28857E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.96           54516           26777           27271
v  Velocity[x]             0.2932          1.9965         0.90807         0.90984
v  Velocity[y]           -0.38229         0.70058      0.00054022      0.00032048
v  Velocity[z]           -0.42092         0.51192       -0.001241      -0.0013614
v  TurbEner             0.0010172        0.015082        0.003286       0.0033455
v  Dissip              9.2064e-05        0.032595      0.00045268       0.0003912
v  TurbVisc               0.16528          11.331          4.7121          5.2733
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              830:        0.91057E-01

===============================================================


 INSTANT    0.831000000E+03   TIME STEP NUMBER             831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999130E+04
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 :  0.23770E+00 0.12496E+01
   Friction velocity        uet   :  0.14214E-01 0.72886E-01
   Friction velocity        uk    :  0.17469E-01 0.38564E-01
   Dimensionless distance   yplus :  0.42916E+03 0.94367E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62933E+01      56   0.14351E-02   0.20641E-01 
c  VelocityX    0.46299E+04      12   0.69445E-02   0.37826E-03 
c  VelocityY    0.46299E+04      12   0.69445E-02   0.34865E-04 
c  VelocityZ    0.46299E+04      12   0.69445E-02   0.58059E-04 
c  TurbEner     0.59749E+01      13   0.13597E-03   0.20577E-08 
c  Dissip       0.14788E+01      16   0.23582E-02   0.73326E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.69           54522           26776           27270
v  Velocity[x]            0.29253          2.0785         0.90804         0.90981
v  Velocity[y]           -0.36609         0.70987      0.00054576      0.00032265
v  Velocity[z]           -0.42185         0.50651      -0.0012467      -0.0013678
v  TurbEner             0.0010146        0.014504       0.0032857       0.0033452
v  Dissip              9.2057e-05        0.031062      0.00045232      0.00039095
v  TurbVisc               0.16551          11.334           4.712          5.2733
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              831:        0.89680E-01

===============================================================


 INSTANT    0.832000000E+03   TIME STEP NUMBER             832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000852E+04
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 :  0.23776E+00 0.13247E+01
   Friction velocity        uet   :  0.14218E-01 0.78950E-01
   Friction velocity        uk    :  0.17447E-01 0.38555E-01
   Dimensionless distance   yplus :  0.42899E+03 0.94372E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64024E+01      55   0.14324E-02   0.20982E-01 
c  VelocityX    0.46297E+04      12   0.67951E-02   0.35996E-03 
c  VelocityY    0.46297E+04      12   0.67951E-02   0.30858E-04 
c  VelocityZ    0.46297E+04      12   0.67951E-02   0.42699E-04 
c  TurbEner     0.59748E+01      13   0.72265E-04   0.79509E-09 
c  Dissip       0.14728E+01      14   0.93575E-03   0.91251E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.01           54533           26776           27271
v  Velocity[x]            0.29259          2.1347         0.90805         0.90983
v  Velocity[y]           -0.38223         0.69678      0.00054096      0.00032011
v  Velocity[z]           -0.42155         0.51104      -0.0012537      -0.0013756
v  TurbEner             0.0010155        0.014342       0.0032855       0.0033451
v  Dissip              9.2051e-05        0.030418      0.00045211       0.0003908
v  TurbVisc               0.16528          11.367          4.7119          5.2732
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              832:        0.89201E-01

===============================================================


 INSTANT    0.833000000E+03   TIME STEP NUMBER             833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998637E+04
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 :  0.23799E+00 0.12191E+01
   Friction velocity        uet   :  0.14231E-01 0.72652E-01
   Friction velocity        uk    :  0.17454E-01 0.38492E-01
   Dimensionless distance   yplus :  0.42834E+03 0.94325E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67461E+01      53   0.13926E-02   0.22109E-01 
c  VelocityX    0.46298E+04      12   0.74533E-02   0.36248E-03 
c  VelocityY    0.46298E+04      12   0.74533E-02   0.39066E-04 
c  VelocityZ    0.46298E+04      12   0.74533E-02   0.91603E-04 
c  TurbEner     0.59755E+01      12   0.66434E-04   0.62777E-09 
c  Dissip       0.14822E+01      14   0.49236E-03   0.55268E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.62           54540           26776           27270
v  Velocity[x]            0.29294          2.1828         0.90805         0.90983
v  Velocity[y]            -0.3677         0.70701       0.0005486      0.00032398
v  Velocity[z]           -0.41934         0.50421      -0.0012454      -0.0013659
v  TurbEner             0.0010169        0.014419       0.0032855       0.0033451
v  Dissip              9.2082e-05        0.030357      0.00045213      0.00039081
v  TurbVisc               0.16494          11.348          4.7119          5.2731
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              833:        0.89185E-01

===============================================================


 INSTANT    0.834000000E+03   TIME STEP NUMBER             834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001246E+04
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 :  0.23738E+00 0.13235E+01
   Friction velocity        uet   :  0.14195E-01 0.78865E-01
   Friction velocity        uk    :  0.17467E-01 0.38463E-01
   Dimensionless distance   yplus :  0.42912E+03 0.94351E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65479E+01      58   0.14761E-02   0.21473E-01 
c  VelocityX    0.46297E+04      12   0.74999E-02   0.37160E-03 
c  VelocityY    0.46297E+04      12   0.74999E-02   0.28731E-04 
c  VelocityZ    0.46297E+04      12   0.74999E-02   0.45125E-04 
c  TurbEner     0.59763E+01      13   0.13398E-03   0.16243E-08 
c  Dissip       0.14921E+01      16   0.19638E-02   0.39050E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.67           54548           26777           27271
v  Velocity[x]             0.2928          2.0195         0.90807         0.90984
v  Velocity[y]           -0.38249         0.70176      0.00053589      0.00031371
v  Velocity[z]           -0.41978         0.51165      -0.0012621      -0.0013855
v  TurbEner             0.0010128         0.01505       0.0032856       0.0033452
v  Dissip              9.2111e-05         0.03186      0.00045223      0.00039091
v  TurbVisc               0.16534           11.35          4.7118          5.2731
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              834:        0.91460E-01

===============================================================


 INSTANT    0.835000000E+03   TIME STEP NUMBER             835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998602E+04
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 :  0.23807E+00 0.12239E+01
   Friction velocity        uet   :  0.14236E-01 0.72348E-01
   Friction velocity        uk    :  0.17431E-01 0.38516E-01
   Dimensionless distance   yplus :  0.42857E+03 0.94329E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65341E+01      56   0.15726E-02   0.21409E-01 
c  VelocityX    0.46298E+04      12   0.73831E-02   0.40396E-03 
c  VelocityY    0.46298E+04      12   0.73831E-02   0.31139E-04 
c  VelocityZ    0.46298E+04      12   0.73831E-02   0.58578E-04 
c  TurbEner     0.59755E+01      13   0.11958E-03   0.16787E-08 
c  Dissip       0.14604E+01      16   0.21676E-02   0.66795E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.59           54540           26776           27270
v  Velocity[x]            0.29288          2.0946         0.90806         0.90983
v  Velocity[y]           -0.36658         0.70987      0.00055402      0.00033074
v  Velocity[z]           -0.42093         0.50598      -0.0012488      -0.0013712
v  TurbEner             0.0010152        0.014544       0.0032854        0.003345
v  Dissip              9.2128e-05         0.03051      0.00045195      0.00039072
v  TurbVisc               0.16489           11.32          4.7118          5.2731
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              835:        0.90208E-01

===============================================================


 INSTANT    0.836000000E+03   TIME STEP NUMBER             836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001195E+04
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 :  0.23796E+00 0.13254E+01
   Friction velocity        uet   :  0.14230E-01 0.78990E-01
   Friction velocity        uk    :  0.17452E-01 0.38565E-01
   Dimensionless distance   yplus :  0.42832E+03 0.94331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68190E+01      64   0.15722E-02   0.22351E-01 
c  VelocityX    0.46298E+04      12   0.68580E-02   0.43301E-03 
c  VelocityY    0.46298E+04      12   0.68580E-02   0.40048E-04 
c  VelocityZ    0.46298E+04      12   0.68580E-02   0.47664E-04 
c  TurbEner     0.59761E+01      13   0.81896E-04   0.12975E-08 
c  Dissip       0.14591E+01      14   0.54859E-03   0.47514E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.2           54515           26777           27271
v  Velocity[x]            0.29277          2.1421         0.90808         0.90986
v  Velocity[y]           -0.38224         0.70012      0.00054513      0.00032579
v  Velocity[z]           -0.42144         0.51109      -0.0012414       -0.001364
v  TurbEner             0.0010152        0.014478       0.0032856       0.0033452
v  Dissip              9.2099e-05        0.030197      0.00045188      0.00039068
v  TurbVisc               0.16477          11.314          4.7117           5.273
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              836:        0.91550E-01

===============================================================


 INSTANT    0.837000000E+03   TIME STEP NUMBER             837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998790E+04
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 :  0.23743E+00 0.12365E+01
   Friction velocity        uet   :  0.14198E-01 0.72543E-01
   Friction velocity        uk    :  0.17451E-01 0.38585E-01
   Dimensionless distance   yplus :  0.42880E+03 0.94292E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59629E+01      57   0.12431E-02   0.19561E-01 
c  VelocityX    0.46299E+04      12   0.65010E-02   0.36850E-03 
c  VelocityY    0.46299E+04      12   0.65010E-02   0.34003E-04 
c  VelocityZ    0.46299E+04      12   0.65010E-02   0.35874E-04 
c  TurbEner     0.59764E+01      13   0.83647E-04   0.12890E-08 
c  Dissip       0.14843E+01      15   0.74739E-03   0.12959E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.53           54523           26776           27270
v  Velocity[x]            0.29256          2.1868         0.90805         0.90982
v  Velocity[y]           -0.36695         0.70649      0.00054913       0.0003246
v  Velocity[z]            -0.4207         0.50474      -0.0012471      -0.0013697
v  TurbEner             0.0010116        0.014612       0.0032856       0.0033452
v  Dissip              9.2067e-05        0.030461      0.00045199      0.00039075
v  TurbVisc               0.16497          11.352          4.7118           5.273
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              837:        0.89609E-01

===============================================================


 INSTANT    0.838000000E+03   TIME STEP NUMBER             838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000933E+04
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 :  0.23803E+00 0.13252E+01
   Friction velocity        uet   :  0.14234E-01 0.78971E-01
   Friction velocity        uk    :  0.17421E-01 0.38601E-01
   Dimensionless distance   yplus :  0.42845E+03 0.94304E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56015E+01      55   0.13583E-02   0.18364E-01 
c  VelocityX    0.46298E+04      13   0.66911E-02   0.33177E-03 
c  VelocityY    0.46298E+04      13   0.66911E-02   0.26461E-04 
c  VelocityZ    0.46298E+04      13   0.66911E-02   0.32121E-04 
c  TurbEner     0.59765E+01      13   0.11849E-03   0.14615E-08 
c  Dissip       0.14948E+01      16   0.19282E-02   0.41375E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.19           54534           26777           27271
v  Velocity[x]            0.29276          2.0201         0.90806         0.90984
v  Velocity[y]           -0.38244         0.70015      0.00054699       0.0003254
v  Velocity[z]           -0.42179          0.5118      -0.0012521      -0.0013761
v  TurbEner             0.0010114        0.015191       0.0032856       0.0033452
v  Dissip              9.2089e-05        0.031934      0.00045211      0.00039085
v  TurbVisc               0.16451          11.339          4.7117          5.2729
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              838:        0.90446E-01

===============================================================


 INSTANT    0.839000000E+03   TIME STEP NUMBER             839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998659E+04
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 :  0.23783E+00 0.12186E+01
   Friction velocity        uet   :  0.14222E-01 0.72312E-01
   Friction velocity        uk    :  0.17419E-01 0.38589E-01
   Dimensionless distance   yplus :  0.42758E+03 0.94321E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61351E+01      60   0.12820E-02   0.20097E-01 
c  VelocityX    0.46298E+04      12   0.72809E-02   0.34108E-03 
c  VelocityY    0.46298E+04      12   0.72809E-02   0.23474E-04 
c  VelocityZ    0.46298E+04      12   0.72809E-02   0.57655E-04 
c  TurbEner     0.59756E+01      13   0.12507E-03   0.16694E-08 
c  Dissip       0.14641E+01      16   0.20442E-02   0.63698E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.69           54539           26776           27270
v  Velocity[x]            0.29311          2.0957         0.90804         0.90982
v  Velocity[y]           -0.36691         0.70848      0.00054886      0.00032518
v  Velocity[z]           -0.41933         0.50565       -0.001253      -0.0013762
v  TurbEner             0.0010116        0.014692       0.0032855       0.0033451
v  Dissip              9.2113e-05        0.030698       0.0004519      0.00039071
v  TurbVisc               0.16414          11.324          4.7116          5.2728
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              839:        0.90319E-01

===============================================================


 INSTANT    0.840000000E+03   TIME STEP NUMBER             840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001602E+04
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 :  0.23749E+00 0.13250E+01
   Friction velocity        uet   :  0.14202E-01 0.78970E-01
   Friction velocity        uk    :  0.17421E-01 0.38476E-01
   Dimensionless distance   yplus :  0.42821E+03 0.94349E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63912E+01      53   0.13211E-02   0.20964E-01 
c  VelocityX    0.46298E+04      12   0.65455E-02   0.31133E-03 
c  VelocityY    0.46298E+04      12   0.65455E-02   0.35249E-04 
c  VelocityZ    0.46298E+04      12   0.65455E-02   0.10245E-03 
c  TurbEner     0.59762E+01      12   0.70507E-04   0.67476E-09 
c  Dissip       0.14701E+01      13   0.59156E-03   0.40651E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.07           54549           26776           27271
v  Velocity[x]            0.29266          2.1535         0.90806         0.90984
v  Velocity[y]           -0.38285         0.69947      0.00054853      0.00032416
v  Velocity[z]           -0.42005         0.51044      -0.0012436      -0.0013688
v  TurbEner             0.0010053        0.014592       0.0032855       0.0033452
v  Dissip              9.2133e-05        0.030311      0.00045187       0.0003907
v  TurbVisc               0.16446          11.356          4.7116          5.2728
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              840:        0.89159E-01

===============================================================


 INSTANT    0.841000000E+03   TIME STEP NUMBER             841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998669E+04
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 :  0.23796E+00 0.12399E+01
   Friction velocity        uet   :  0.14231E-01 0.72506E-01
   Friction velocity        uk    :  0.17366E-01 0.38437E-01
   Dimensionless distance   yplus :  0.42727E+03 0.94369E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58117E+01      56   0.14938E-02   0.19055E-01 
c  VelocityX    0.46298E+04      13   0.71078E-02   0.32280E-03 
c  VelocityY    0.46298E+04      13   0.71078E-02   0.29354E-04 
c  VelocityZ    0.46298E+04      13   0.71078E-02   0.46151E-04 
c  TurbEner     0.59770E+01      12   0.77979E-04   0.84711E-09 
c  Dissip       0.14869E+01      15   0.82266E-03   0.14650E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.42           54540           26776           27270
v  Velocity[x]             0.2925          2.1866         0.90805         0.90983
v  Velocity[y]            -0.3674         0.70625      0.00055956      0.00033362
v  Velocity[z]           -0.42287         0.50437      -0.0012505      -0.0013737
v  TurbEner             0.0010054         0.01478       0.0032855       0.0033452
v  Dissip              9.2156e-05         0.03066      0.00045199      0.00039078
v  TurbVisc               0.16366          11.335          4.7116          5.2728
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              841:        0.89889E-01

===============================================================


 INSTANT    0.842000000E+03   TIME STEP NUMBER             842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001862E+04
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 :  0.23768E+00 0.13250E+01
   Friction velocity        uet   :  0.14213E-01 0.78968E-01
   Friction velocity        uk    :  0.17367E-01 0.38510E-01
   Dimensionless distance   yplus :  0.42656E+03 0.94405E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67560E+01      61   0.15548E-02   0.22141E-01 
c  VelocityX    0.46298E+04      12   0.69220E-02   0.42540E-03 
c  VelocityY    0.46298E+04      12   0.69220E-02   0.39554E-04 
c  VelocityZ    0.46298E+04      12   0.69220E-02   0.47631E-04 
c  TurbEner     0.59781E+01      13   0.86797E-04   0.13015E-08 
c  Dissip       0.15143E+01      15   0.10566E-02   0.20690E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.45           54515           26776           27271
v  Velocity[x]             0.2932          2.2035         0.90808         0.90986
v  Velocity[y]           -0.38227         0.69939      0.00055089      0.00032918
v  Velocity[z]           -0.41901          0.5119      -0.0012313      -0.0013525
v  TurbEner             0.0010036         0.01504       0.0032857       0.0033454
v  Dissip              9.2173e-05        0.031305       0.0004523        0.000391
v  TurbVisc               0.16353          11.328          4.7116          5.2728
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              842:        0.90696E-01

===============================================================


 INSTANT    0.843000000E+03   TIME STEP NUMBER             843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999297E+04
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 :  0.23766E+00 0.12364E+01
   Friction velocity        uet   :  0.14213E-01 0.72330E-01
   Friction velocity        uk    :  0.17351E-01 0.38586E-01
   Dimensionless distance   yplus :  0.42660E+03 0.94373E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69299E+01      59   0.15932E-02   0.22730E-01 
c  VelocityX    0.46298E+04      12   0.60003E-02   0.39068E-03 
c  VelocityY    0.46298E+04      12   0.60003E-02   0.46849E-04 
c  VelocityZ    0.46298E+04      12   0.60003E-02   0.32175E-04 
c  TurbEner     0.59785E+01      13   0.13293E-03   0.17330E-08 
c  Dissip       0.15437E+01      16   0.24186E-02   0.67842E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.74           54522           26776           27270
v  Velocity[x]             0.2927           2.047         0.90804          0.9098
v  Velocity[y]           -0.36611         0.70768      0.00055591      0.00033071
v  Velocity[z]           -0.42076         0.50651      -0.0012494      -0.0013715
v  TurbEner            0.00099958        0.015688       0.0032858       0.0033454
v  Dissip              9.2165e-05        0.033227      0.00045261      0.00039122
v  TurbVisc               0.16364          11.359          4.7116          5.2728
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              843:        0.90338E-01

===============================================================


 INSTANT    0.844000000E+03   TIME STEP NUMBER             844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001021E+04
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 :  0.23795E+00 0.13247E+01
   Friction velocity        uet   :  0.14230E-01 0.78956E-01
   Friction velocity        uk    :  0.17317E-01 0.38598E-01
   Dimensionless distance   yplus :  0.42614E+03 0.94394E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59358E+01      55   0.12728E-02   0.19470E-01 
c  VelocityX    0.46298E+04      12   0.67707E-02   0.31522E-03 
c  VelocityY    0.46298E+04      12   0.67707E-02   0.28352E-04 
c  VelocityZ    0.46298E+04      12   0.67707E-02   0.38771E-04 
c  TurbEner     0.59770E+01      13   0.12732E-03   0.16307E-08 
c  Dissip       0.15171E+01      16   0.18084E-02   0.47271E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.06           54534           26777           27271
v  Velocity[x]            0.29253          2.1111         0.90806         0.90984
v  Velocity[y]           -0.38226         0.69892      0.00054316       0.0003204
v  Velocity[z]           -0.42221         0.51113      -0.0012493      -0.0013702
v  TurbEner             0.0010001        0.015107       0.0032856       0.0033452
v  Dissip              9.2135e-05        0.031997      0.00045247      0.00039111
v  TurbVisc               0.16328          11.348          4.7115          5.2727
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              844:        0.90308E-01

===============================================================


 INSTANT    0.845000000E+03   TIME STEP NUMBER             845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997950E+04
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 :  0.23785E+00 0.12400E+01
   Friction velocity        uet   :  0.14224E-01 0.72468E-01
   Friction velocity        uk    :  0.17321E-01 0.38576E-01
   Dimensionless distance   yplus :  0.42539E+03 0.94439E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55891E+01      62   0.11967E-02   0.18309E-01 
c  VelocityX    0.46298E+04      12   0.72223E-02   0.30454E-03 
c  VelocityY    0.46298E+04      12   0.72223E-02   0.21261E-04 
c  VelocityZ    0.46298E+04      12   0.72223E-02   0.54012E-04 
c  TurbEner     0.59771E+01      12   0.57691E-04   0.51586E-09 
c  Dissip       0.15270E+01      13   0.22736E-03   0.14678E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.88           54541           26776           27271
v  Velocity[x]            0.29304          2.1579         0.90803         0.90981
v  Velocity[y]           -0.36772          0.7058        0.000547       0.0003209
v  Velocity[z]            -0.4208         0.50414      -0.0012435      -0.0013678
v  TurbEner             0.0010024        0.015083       0.0032855       0.0033452
v  Dissip              9.2065e-05        0.032043      0.00045254      0.00039115
v  TurbVisc               0.16318          11.354          4.7114          5.2727
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              845:        0.90580E-01

===============================================================


 INSTANT    0.846000000E+03   TIME STEP NUMBER             846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000669E+04
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 :  0.23782E+00 0.13253E+01
   Friction velocity        uet   :  0.14222E-01 0.78986E-01
   Friction velocity        uk    :  0.17341E-01 0.38395E-01
   Dimensionless distance   yplus :  0.42632E+03 0.94425E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59115E+01      55   0.13006E-02   0.19389E-01 
c  VelocityX    0.46299E+04      13   0.71932E-02   0.34092E-03 
c  VelocityY    0.46299E+04      13   0.71932E-02   0.26711E-04 
c  VelocityZ    0.46299E+04      13   0.71932E-02   0.46899E-04 
c  TurbEner     0.59781E+01      12   0.71268E-04   0.76506E-09 
c  Dissip       0.15517E+01      15   0.82230E-03   0.17686E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.33           54551           26777           27272
v  Velocity[x]            0.29289          2.1919         0.90807         0.90984
v  Velocity[y]           -0.38248         0.69944      0.00053819      0.00031689
v  Velocity[z]             -0.421         0.51174      -0.0012465      -0.0013709
v  TurbEner            0.00099939        0.015141       0.0032855       0.0033451
v  Dissip              9.2097e-05        0.032205      0.00045271      0.00039126
v  TurbVisc               0.16383          11.333          4.7114          5.2727
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              846:        0.90021E-01

===============================================================


 INSTANT    0.847000000E+03   TIME STEP NUMBER             847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998394E+04
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 :  0.23788E+00 0.12135E+01
   Friction velocity        uet   :  0.14226E-01 0.72329E-01
   Friction velocity        uk    :  0.17315E-01 0.38499E-01
   Dimensionless distance   yplus :  0.42590E+03 0.94417E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67894E+01      56   0.18009E-02   0.22248E-01 
c  VelocityX    0.46298E+04      12   0.70103E-02   0.40808E-03 
c  VelocityY    0.46298E+04      12   0.70103E-02   0.34764E-04 
c  VelocityZ    0.46298E+04      12   0.70103E-02   0.95344E-04 
c  TurbEner     0.59786E+01      13   0.10580E-03   0.10214E-08 
c  Dissip       0.15641E+01      16   0.18346E-02   0.40128E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.81           54541           26777           27271
v  Velocity[x]            0.29262          2.0375         0.90805         0.90982
v  Velocity[y]           -0.36664         0.70791      0.00055719      0.00033341
v  Velocity[z]           -0.42287         0.50598      -0.0012448      -0.0013707
v  TurbEner             0.0010035        0.015645       0.0032856       0.0033452
v  Dissip              9.2051e-05        0.033644      0.00045294      0.00039142
v  TurbVisc               0.16362          11.328          4.7114          5.2727
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              847:        0.89468E-01

===============================================================


 INSTANT    0.848000000E+03   TIME STEP NUMBER             848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000628E+04
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 :  0.23749E+00 0.13249E+01
   Friction velocity        uet   :  0.14203E-01 0.78970E-01
   Friction velocity        uk    :  0.17351E-01 0.38593E-01
   Dimensionless distance   yplus :  0.42586E+03 0.94471E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71318E+01      62   0.16006E-02   0.23387E-01 
c  VelocityX    0.46298E+04      12   0.64527E-02   0.40160E-03 
c  VelocityY    0.46298E+04      12   0.64527E-02   0.26578E-04 
c  VelocityZ    0.46298E+04      12   0.64527E-02   0.49330E-04 
c  TurbEner     0.59776E+01      13   0.13086E-03   0.20900E-08 
c  Dissip       0.15298E+01      16   0.20487E-02   0.67455E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.18           54516           26777           27272
v  Velocity[x]            0.29297          2.0979         0.90805         0.90984
v  Velocity[y]            -0.3823         0.69762      0.00055516      0.00033395
v  Velocity[z]           -0.41986         0.51101      -0.0012295       -0.001353
v  TurbEner             0.0010057        0.015114       0.0032856       0.0033452
v  Dissip              9.2053e-05        0.032368      0.00045275      0.00039129
v  TurbVisc               0.16372          11.357          4.7114          5.2726
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              848:        0.91327E-01

===============================================================


 INSTANT    0.849000000E+03   TIME STEP NUMBER             849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999704E+04
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 :  0.23745E+00 0.12260E+01
   Friction velocity        uet   :  0.14200E-01 0.72610E-01
   Friction velocity        uk    :  0.17369E-01 0.38607E-01
   Dimensionless distance   yplus :  0.42668E+03 0.94445E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60180E+01      54   0.11838E-02   0.19732E-01 
c  VelocityX    0.46299E+04      12   0.65834E-02   0.32851E-03 
c  VelocityY    0.46299E+04      12   0.65834E-02   0.31282E-04 
c  VelocityZ    0.46299E+04      12   0.65834E-02   0.31525E-04 
c  TurbEner     0.59770E+01      13   0.69667E-04   0.99406E-09 
c  Dissip       0.15378E+01      14   0.44869E-03   0.38121E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.95           54523           26777           27271
v  Velocity[x]            0.29261          2.1631         0.90804         0.90981
v  Velocity[y]             -0.367         0.70536      0.00055411      0.00032824
v  Velocity[z]           -0.42017         0.50474      -0.0012423      -0.0013659
v  TurbEner             0.0010047        0.014952       0.0032854        0.003345
v  Dissip              9.2034e-05        0.032131      0.00045269      0.00039124
v  TurbVisc                0.1642          11.339          4.7114          5.2727
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              849:        0.89222E-01

===============================================================


 INSTANT    0.850000000E+03   TIME STEP NUMBER             850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001703E+04
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 :  0.23795E+00 0.13244E+01
   Friction velocity        uet   :  0.14231E-01 0.78931E-01
   Friction velocity        uk    :  0.17361E-01 0.38555E-01
   Dimensionless distance   yplus :  0.42680E+03 0.94457E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60910E+01      52   0.13003E-02   0.19962E-01 
c  VelocityX    0.46298E+04      12   0.75491E-02   0.33519E-03 
c  VelocityY    0.46298E+04      12   0.75491E-02   0.25053E-04 
c  VelocityZ    0.46298E+04      12   0.75491E-02   0.46455E-04 
c  TurbEner     0.59773E+01      13   0.73720E-04   0.83912E-09 
c  Dissip       0.15598E+01      15   0.80083E-03   0.14925E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.01           54533           26777           27271
v  Velocity[x]            0.29271          2.1884         0.90806         0.90984
v  Velocity[y]           -0.38247          0.7024      0.00054155      0.00032089
v  Velocity[z]           -0.42097         0.51171      -0.0012486      -0.0013692
v  TurbEner             0.0010068        0.015038       0.0032852       0.0033449
v  Dissip              9.2038e-05        0.032437      0.00045279       0.0003913
v  TurbVisc               0.16416          11.353          4.7113          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              850:        0.88658E-01

===============================================================


 INSTANT    0.851000000E+03   TIME STEP NUMBER             851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001414E+04
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 :  0.23805E+00 0.12140E+01
   Friction velocity        uet   :  0.14236E-01 0.72358E-01
   Friction velocity        uk    :  0.17379E-01 0.38552E-01
   Dimensionless distance   yplus :  0.42642E+03 0.94521E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75018E+01      60   0.14991E-02   0.24586E-01 
c  VelocityX    0.46298E+04      12   0.69590E-02   0.42630E-03 
c  VelocityY    0.46298E+04      12   0.69590E-02   0.25311E-04 
c  VelocityZ    0.46298E+04      12   0.69590E-02   0.11379E-03 
c  TurbEner     0.59773E+01      12   0.11864E-03   0.10122E-08 
c  Dissip       0.15722E+01      16   0.19515E-02   0.41475E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.97           54540           26775           27270
v  Velocity[x]            0.29303          2.0255         0.90804         0.90981
v  Velocity[y]           -0.36694         0.71078      0.00055703      0.00033159
v  Velocity[z]            -0.4215         0.50564      -0.0012459      -0.0013691
v  TurbEner              0.001009        0.015597       0.0032852       0.0033448
v  Dissip              9.2051e-05        0.033984      0.00045294       0.0003914
v  TurbVisc               0.16395          11.335          4.7112          5.2726
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              851:        0.90300E-01

===============================================================


 INSTANT    0.852000000E+03   TIME STEP NUMBER             852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001989E+04
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 :  0.23777E+00 0.13250E+01
   Friction velocity        uet   :  0.14220E-01 0.78976E-01
   Friction velocity        uk    :  0.17398E-01 0.38484E-01
   Dimensionless distance   yplus :  0.42743E+03 0.94515E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65071E+01      65   0.13748E-02   0.21346E-01 
c  VelocityX    0.46297E+04      13   0.64833E-02   0.35340E-03 
c  VelocityY    0.46297E+04      13   0.64833E-02   0.44411E-04 
c  VelocityZ    0.46297E+04      13   0.64833E-02   0.48882E-04 
c  TurbEner     0.59757E+01      13   0.15062E-03   0.19930E-08 
c  Dissip       0.15299E+01      16   0.24854E-02   0.83970E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.12           54549           26777           27271
v  Velocity[x]             0.2926          2.0926         0.90808         0.90985
v  Velocity[y]           -0.38283         0.69789      0.00054182      0.00032104
v  Velocity[z]            -0.4222         0.51051      -0.0012564      -0.0013768
v  TurbEner              0.001005        0.014929       0.0032849       0.0033446
v  Dissip              9.2043e-05        0.032306      0.00045265      0.00039119
v  TurbVisc               0.16445          11.341          4.7112          5.2725
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              852:        0.92365E-01

===============================================================


 INSTANT    0.853000000E+03   TIME STEP NUMBER             853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998194E+04
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 :  0.23781E+00 0.12406E+01
   Friction velocity        uet   :  0.14223E-01 0.72634E-01
   Friction velocity        uk    :  0.17364E-01 0.38565E-01
   Dimensionless distance   yplus :  0.42700E+03 0.94538E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70469E+01      56   0.15623E-02   0.23091E-01 
c  VelocityX    0.46298E+04      12   0.75260E-02   0.36476E-03 
c  VelocityY    0.46298E+04      12   0.75260E-02   0.39954E-04 
c  VelocityZ    0.46298E+04      12   0.75260E-02   0.30446E-04 
c  TurbEner     0.59763E+01      13   0.73921E-04   0.99428E-09 
c  Dissip       0.15295E+01      14   0.60284E-03   0.44054E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.51           54540           26776           27270
v  Velocity[x]            0.29275          2.1575         0.90806         0.90983
v  Velocity[y]           -0.36731         0.70644      0.00054768      0.00032452
v  Velocity[z]           -0.42209         0.50436      -0.0012502      -0.0013712
v  TurbEner             0.0010073        0.014755        0.003285       0.0033446
v  Dissip              9.2084e-05        0.031888       0.0004526      0.00039115
v  TurbVisc                 0.164          11.302          4.7111          5.2724
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              853:        0.89490E-01

===============================================================


 INSTANT    0.854000000E+03   TIME STEP NUMBER             854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000379E+04
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 :  0.23785E+00 0.13245E+01
   Friction velocity        uet   :  0.14225E-01 0.78931E-01
   Friction velocity        uk    :  0.17384E-01 0.38607E-01
   Dimensionless distance   yplus :  0.42680E+03 0.94540E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66535E+01      56   0.15467E-02   0.21804E-01 
c  VelocityX    0.46298E+04      12   0.71192E-02   0.44891E-03 
c  VelocityY    0.46298E+04      12   0.71192E-02   0.30446E-04 
c  VelocityZ    0.46298E+04      12   0.71192E-02   0.52239E-04 
c  TurbEner     0.59770E+01      13   0.78100E-04   0.13626E-08 
c  Dissip       0.15475E+01      15   0.66075E-03   0.10486E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.23           54514           26776           27271
v  Velocity[x]            0.29279          2.1804         0.90807         0.90984
v  Velocity[y]            -0.3822         0.70195      0.00054565      0.00032703
v  Velocity[z]           -0.41929         0.51194      -0.0012452      -0.0013637
v  TurbEner             0.0010073        0.014881       0.0032852       0.0033448
v  Dissip              9.2056e-05         0.03213      0.00045274      0.00039125
v  TurbVisc               0.16399          11.293          4.7112          5.2725
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              854:        0.89170E-01

===============================================================


 INSTANT    0.855000000E+03   TIME STEP NUMBER             855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998730E+04
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 :  0.23741E+00 0.12402E+01
   Friction velocity        uet   :  0.14198E-01 0.72608E-01
   Friction velocity        uk    :  0.17383E-01 0.38528E-01
   Dimensionless distance   yplus :  0.42731E+03 0.94463E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62014E+01      53   0.13955E-02   0.20337E-01 
c  VelocityX    0.46298E+04      12   0.66409E-02   0.40767E-03 
c  VelocityY    0.46298E+04      12   0.66409E-02   0.35385E-04 
c  VelocityZ    0.46298E+04      12   0.66409E-02   0.10787E-03 
c  TurbEner     0.59769E+01      13   0.12758E-03   0.16594E-08 
c  Dissip       0.15562E+01      15   0.18561E-02   0.36494E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.43           54519           26776           27270
v  Velocity[x]            0.29275          2.0204         0.90806         0.90983
v  Velocity[y]           -0.36606         0.70982      0.00055295       0.0003269
v  Velocity[z]              -0.42         0.50652      -0.0012428      -0.0013632
v  TurbEner             0.0010042        0.015458       0.0032853       0.0033448
v  Dissip              9.2023e-05         0.03359       0.0004529      0.00039136
v  TurbVisc               0.16427           11.32          4.7112          5.2725
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              855:        0.89039E-01

===============================================================


 INSTANT    0.856000000E+03   TIME STEP NUMBER             856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001376E+04
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 :  0.23783E+00 0.13240E+01
   Friction velocity        uet   :  0.14223E-01 0.78915E-01
   Friction velocity        uk    :  0.17357E-01 0.38568E-01
   Dimensionless distance   yplus :  0.42706E+03 0.94410E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54112E+01      53   0.11533E-02   0.17742E-01 
c  VelocityX    0.46297E+04      12   0.70282E-02   0.35809E-03 
c  VelocityY    0.46297E+04      12   0.70282E-02   0.26783E-04 
c  VelocityZ    0.46297E+04      12   0.70282E-02   0.52707E-04 
c  TurbEner     0.59757E+01      14   0.14949E-03   0.22640E-08 
c  Dissip       0.15173E+01      16   0.24015E-02   0.76487E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.11           54523           26777           27271
v  Velocity[x]            0.29287          2.0964         0.90805         0.90982
v  Velocity[y]           -0.38228         0.70101       0.0005504      0.00032932
v  Velocity[z]           -0.42111         0.51105      -0.0012461      -0.0013698
v  TurbEner              0.001005        0.014826       0.0032852       0.0033447
v  Dissip              9.1978e-05        0.031968      0.00045258      0.00039114
v  TurbVisc               0.16392          11.369          4.7111          5.2724
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              856:        0.89331E-01

===============================================================


 INSTANT    0.857000000E+03   TIME STEP NUMBER             857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998972E+04
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 :  0.23795E+00 0.12176E+01
   Friction velocity        uet   :  0.14231E-01 0.72575E-01
   Friction velocity        uk    :  0.17363E-01 0.38590E-01
   Dimensionless distance   yplus :  0.42634E+03 0.94293E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58596E+01      65   0.13886E-02   0.19211E-01 
c  VelocityX    0.46298E+04      12   0.68164E-02   0.33585E-03 
c  VelocityY    0.46298E+04      12   0.68164E-02   0.24402E-04 
c  VelocityZ    0.46298E+04      12   0.68164E-02   0.27943E-04 
c  TurbEner     0.59757E+01      12   0.65147E-04   0.70828E-09 
c  Dissip       0.15163E+01      13   0.52637E-03   0.36884E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.12           54504           26776           27270
v  Velocity[x]            0.29307          2.1432         0.90806         0.90984
v  Velocity[y]           -0.36774         0.70817      0.00055601      0.00033283
v  Velocity[z]           -0.42177         0.50424      -0.0012401      -0.0013586
v  TurbEner             0.0010069        0.014684       0.0032851       0.0033447
v  Dissip              9.2019e-05        0.031631       0.0004525      0.00039108
v  TurbVisc               0.16376          11.356          4.7112          5.2724
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              857:        0.92801E-01

===============================================================


 INSTANT    0.858000000E+03   TIME STEP NUMBER             858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000635E+04
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 :  0.23740E+00 0.13261E+01
   Friction velocity        uet   :  0.14198E-01 0.79025E-01
   Friction velocity        uk    :  0.17380E-01 0.38540E-01
   Dimensionless distance   yplus :  0.42728E+03 0.94245E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56009E+01      54   0.13503E-02   0.18362E-01 
c  VelocityX    0.46298E+04      12   0.71604E-02   0.31687E-03 
c  VelocityY    0.46298E+04      12   0.71604E-02   0.21617E-04 
c  VelocityZ    0.46298E+04      12   0.71604E-02   0.54909E-04 
c  TurbEner     0.59758E+01      13   0.74862E-04   0.11147E-08 
c  Dissip       0.15336E+01      15   0.64342E-03   0.89718E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.37           54515           26776           27270
v  Velocity[x]            0.29251          2.1758         0.90804         0.90982
v  Velocity[y]           -0.38253         0.70241      0.00055045      0.00032702
v  Velocity[z]           -0.42078         0.51166      -0.0012434      -0.0013675
v  TurbEner             0.0010028          0.0148       0.0032851       0.0033447
v  Dissip               9.208e-05        0.031949      0.00045254      0.00039111
v  TurbVisc               0.16431           11.36          4.7111          5.2723
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              858:        0.89632E-01

===============================================================


 INSTANT    0.859000000E+03   TIME STEP NUMBER             859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999043E+04
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 :  0.23798E+00 0.12143E+01
   Friction velocity        uet   :  0.14233E-01 0.72371E-01
   Friction velocity        uk    :  0.17345E-01 0.38549E-01
   Dimensionless distance   yplus :  0.42671E+03 0.94205E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56796E+01      58   0.11978E-02   0.18616E-01 
c  VelocityX    0.46298E+04      12   0.71197E-02   0.32418E-03 
c  VelocityY    0.46298E+04      12   0.71197E-02   0.27883E-04 
c  VelocityZ    0.46298E+04      12   0.71197E-02   0.44548E-04 
c  TurbEner     0.59765E+01      13   0.72758E-04   0.88709E-09 
c  Dissip       0.15599E+01      15   0.81923E-03   0.14412E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.89           54530           26775           27270
v  Velocity[x]            0.29266          2.1996         0.90805         0.90983
v  Velocity[y]           -0.36652         0.70946      0.00055465      0.00032846
v  Velocity[z]           -0.42199         0.50599      -0.0012519       -0.001373
v  TurbEner             0.0010052        0.014954       0.0032849       0.0033445
v  Dissip              9.2114e-05        0.032342      0.00045262      0.00039116
v  TurbVisc               0.16385          11.336          4.7111          5.2724
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              859:        0.90014E-01

===============================================================


 INSTANT    0.860000000E+03   TIME STEP NUMBER             860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001544E+04
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 :  0.23787E+00 0.13257E+01
   Friction velocity        uet   :  0.14226E-01 0.79016E-01
   Friction velocity        uk    :  0.17366E-01 0.38549E-01
   Dimensionless distance   yplus :  0.42638E+03 0.94202E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62517E+01      54   0.14039E-02   0.20492E-01 
c  VelocityX    0.46297E+04      12   0.69309E-02   0.35471E-03 
c  VelocityY    0.46297E+04      12   0.69309E-02   0.48121E-04 
c  VelocityZ    0.46297E+04      12   0.69309E-02   0.82894E-04 
c  TurbEner     0.59770E+01      13   0.12104E-03   0.12081E-08 
c  Dissip       0.15764E+01      16   0.21047E-02   0.49376E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.66           54540           26776           27270
v  Velocity[x]             0.2932          2.0393         0.90804         0.90981
v  Velocity[y]           -0.38218         0.69798      0.00055093      0.00032712
v  Velocity[z]           -0.41839          0.5111      -0.0012452      -0.0013712
v  TurbEner             0.0010053        0.015546       0.0032849       0.0033446
v  Dissip              9.2096e-05        0.033998      0.00045282      0.00039131
v  TurbVisc                0.1638          11.331           4.711          5.2722
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              860:        0.95379E-01

===============================================================


 INSTANT    0.861000000E+03   TIME STEP NUMBER             861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999602E+04
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 :  0.23761E+00 0.12601E+01
   Friction velocity        uet   :  0.14210E-01 0.73494E-01
   Friction velocity        uk    :  0.17367E-01 0.38497E-01
   Dimensionless distance   yplus :  0.42678E+03 0.94212E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59606E+01      57   0.12593E-02   0.19548E-01 
c  VelocityX    0.46297E+04      12   0.66319E-02   0.35479E-03 
c  VelocityY    0.46297E+04      12   0.66319E-02   0.27122E-04 
c  VelocityZ    0.46297E+04      12   0.66319E-02   0.42319E-04 
c  TurbEner     0.59759E+01      13   0.12876E-03   0.16120E-08 
c  Dissip       0.15436E+01      16   0.21210E-02   0.66717E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.29           54548           26776           27270
v  Velocity[x]            0.29261          2.1033         0.90805         0.90982
v  Velocity[y]           -0.36692         0.70631      0.00054006      0.00031553
v  Velocity[z]           -0.42044         0.50473      -0.0012525      -0.0013717
v  TurbEner             0.0010025        0.015001       0.0032847       0.0033445
v  Dissip              9.2113e-05        0.032629      0.00045258      0.00039115
v  TurbVisc               0.16402          11.364           4.711          5.2723
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              861:        0.89568E-01

===============================================================


 INSTANT    0.862000000E+03   TIME STEP NUMBER             862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998169E+04
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 :  0.23773E+00 0.13239E+01
   Friction velocity        uet   :  0.14217E-01 0.78901E-01
   Friction velocity        uk    :  0.17342E-01 0.38522E-01
   Dimensionless distance   yplus :  0.42658E+03 0.94244E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62043E+01      53   0.14115E-02   0.20327E-01 
c  VelocityX    0.46297E+04      12   0.72625E-02   0.36625E-03 
c  VelocityY    0.46297E+04      12   0.72625E-02   0.22534E-04 
c  VelocityZ    0.46297E+04      12   0.72625E-02   0.33843E-04 
c  TurbEner     0.59765E+01      13   0.63986E-04   0.64158E-09 
c  Dissip       0.15445E+01      13   0.51420E-03   0.36302E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.56           54541           26776           27270
v  Velocity[x]             0.2924          2.1626         0.90806         0.90983
v  Velocity[y]           -0.38239         0.70248      0.00055025      0.00033023
v  Velocity[z]           -0.42185          0.5118       -0.001244      -0.0013666
v  TurbEner             0.0010032        0.014852       0.0032848       0.0033446
v  Dissip              9.2113e-05        0.032302      0.00045256      0.00039114
v  TurbVisc               0.16372          11.346          4.7109          5.2722
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              862:        0.88780E-01

===============================================================


 INSTANT    0.863000000E+03   TIME STEP NUMBER             863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999106E+04
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 :  0.23774E+00 0.12133E+01
   Friction velocity        uet   :  0.14218E-01 0.72309E-01
   Friction velocity        uk    :  0.17348E-01 0.38559E-01
   Dimensionless distance   yplus :  0.42591E+03 0.94299E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63497E+01      59   0.15179E-02   0.20812E-01 
c  VelocityX    0.46298E+04      12   0.70120E-02   0.41361E-03 
c  VelocityY    0.46298E+04      12   0.70120E-02   0.33305E-04 
c  VelocityZ    0.46298E+04      12   0.70120E-02   0.39172E-04 
c  TurbEner     0.59776E+01      13   0.87267E-04   0.12680E-08 
c  Dissip       0.15663E+01      15   0.67242E-03   0.11225E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.84           54516           26776           27270
v  Velocity[x]            0.29292          2.1858         0.90807         0.90984
v  Velocity[y]           -0.36682         0.71026      0.00055646      0.00033387
v  Velocity[z]           -0.42049         0.50574      -0.0012382      -0.0013591
v  TurbEner             0.0010048        0.014975       0.0032849       0.0033447
v  Dissip              9.2117e-05        0.032531      0.00045274      0.00039126
v  TurbVisc               0.16347           11.36           4.711          5.2723
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              863:        0.89503E-01

===============================================================


 INSTANT    0.864000000E+03   TIME STEP NUMBER             864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000864E+04
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 :  0.23777E+00 0.13250E+01
   Friction velocity        uet   :  0.14220E-01 0.78969E-01
   Friction velocity        uk    :  0.17362E-01 0.38473E-01
   Dimensionless distance   yplus :  0.42677E+03 0.94331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59175E+01      54   0.13762E-02   0.19406E-01 
c  VelocityX    0.46297E+04      12   0.69814E-02   0.37066E-03 
c  VelocityY    0.46297E+04      12   0.69814E-02   0.47576E-04 
c  VelocityZ    0.46297E+04      12   0.69814E-02   0.10044E-03 
c  TurbEner     0.59774E+01      13   0.12913E-03   0.16273E-08 
c  Dissip       0.15747E+01      16   0.19370E-02   0.40643E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.93           54525           26776           27270
v  Velocity[x]            0.29277          2.0202         0.90803         0.90981
v  Velocity[y]           -0.38283         0.69695      0.00056027      0.00033434
v  Velocity[z]           -0.42081         0.51044      -0.0012407      -0.0013664
v  TurbEner             0.0010002        0.015596        0.003285       0.0033448
v  Dissip              9.2066e-05        0.034058      0.00045291       0.0003914
v  TurbVisc               0.16393          11.336           4.711          5.2722
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              864:        0.89185E-01

===============================================================


 INSTANT    0.865000000E+03   TIME STEP NUMBER             865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000890E+04
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 :  0.23784E+00 0.12625E+01
   Friction velocity        uet   :  0.14225E-01 0.73635E-01
   Friction velocity        uk    :  0.17322E-01 0.38477E-01
   Dimensionless distance   yplus :  0.42608E+03 0.94309E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59095E+01      53   0.11830E-02   0.19373E-01 
c  VelocityX    0.46297E+04      13   0.66128E-02   0.34492E-03 
c  VelocityY    0.46297E+04      13   0.66128E-02   0.24999E-04 
c  VelocityZ    0.46297E+04      13   0.66128E-02   0.46922E-04 
c  TurbEner     0.59759E+01      13   0.14811E-03   0.19218E-08 
c  Dissip       0.15305E+01      16   0.25950E-02   0.89662E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.31           54535           26776           27270
v  Velocity[x]            0.29288          2.0986         0.90805         0.90983
v  Velocity[y]           -0.36733          0.7066       0.0005524      0.00032786
v  Velocity[z]           -0.42271         0.50444      -0.0012519      -0.0013744
v  TurbEner             0.0010025        0.014919       0.0032848       0.0033446
v  Dissip              9.2088e-05        0.032295      0.00045263       0.0003912
v  TurbVisc               0.16335          11.334          4.7109          5.2722
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              865:        0.89823E-01

===============================================================


 INSTANT    0.866000000E+03   TIME STEP NUMBER             866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998922E+04
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 :  0.23766E+00 0.13236E+01
   Friction velocity        uet   :  0.14214E-01 0.78867E-01
   Friction velocity        uk    :  0.17342E-01 0.38514E-01
   Dimensionless distance   yplus :  0.42571E+03 0.94322E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60196E+01      54   0.11550E-02   0.19726E-01 
c  VelocityX    0.46297E+04      12   0.64715E-02   0.37902E-03 
c  VelocityY    0.46297E+04      12   0.64715E-02   0.25334E-04 
c  VelocityZ    0.46297E+04      12   0.64715E-02   0.31693E-04 
c  TurbEner     0.59763E+01      12   0.66014E-04   0.63469E-09 
c  Dissip       0.15283E+01      13   0.58065E-03   0.39440E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.29           54540           26776           27270
v  Velocity[x]            0.29288          2.1558         0.90806         0.90984
v  Velocity[y]           -0.38215         0.70119      0.00054837      0.00032613
v  Velocity[z]           -0.41865         0.51195      -0.0012437      -0.0013683
v  TurbEner             0.0010029        0.014781       0.0032849       0.0033447
v  Dissip              9.2138e-05        0.031888       0.0004526      0.00039119
v  TurbVisc                0.1633          11.364          4.7108          5.2722
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              866:        0.89024E-01

===============================================================


 INSTANT    0.867000000E+03   TIME STEP NUMBER             867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000474E+04
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 :  0.23756E+00 0.12171E+01
   Friction velocity        uet   :  0.14209E-01 0.72538E-01
   Friction velocity        uk    :  0.17345E-01 0.38555E-01
   Dimensionless distance   yplus :  0.42618E+03 0.94304E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62083E+01      57   0.13448E-02   0.20362E-01 
c  VelocityX    0.46298E+04      12   0.71670E-02   0.42178E-03 
c  VelocityY    0.46298E+04      12   0.71670E-02   0.22446E-04 
c  VelocityZ    0.46298E+04      12   0.71670E-02   0.44004E-04 
c  TurbEner     0.59766E+01      13   0.95873E-04   0.92879E-09 
c  Dissip       0.15296E+01      15   0.13839E-02   0.22956E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.95           54549           26776           27270
v  Velocity[x]            0.29265          1.9991         0.90807         0.90984
v  Velocity[y]           -0.36601          0.7093      0.00054334      0.00031893
v  Velocity[z]           -0.42053         0.50658      -0.0012666      -0.0013856
v  TurbEner             0.0010007        0.015203        0.003285       0.0033448
v  Dissip              9.2153e-05        0.032899      0.00045268      0.00039125
v  TurbVisc               0.16358          11.347           4.711          5.2723
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              867:        0.89478E-01

===============================================================


 INSTANT    0.868000000E+03   TIME STEP NUMBER             868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001106E+04
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 :  0.23768E+00 0.13236E+01
   Friction velocity        uet   :  0.14217E-01 0.78878E-01
   Friction velocity        uk    :  0.17326E-01 0.38593E-01
   Dimensionless distance   yplus :  0.42604E+03 0.94354E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70159E+01      56   0.16758E-02   0.22997E-01 
c  VelocityX    0.46297E+04      12   0.70771E-02   0.38677E-03 
c  VelocityY    0.46297E+04      12   0.70771E-02   0.58149E-04 
c  VelocityZ    0.46297E+04      12   0.70771E-02   0.12511E-03 
c  TurbEner     0.59756E+01      13   0.13854E-03   0.19188E-08 
c  Dissip       0.14839E+01      17   0.28143E-02   0.10204E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.34           54540           26776           27270
v  Velocity[x]            0.29274          2.0843         0.90805         0.90983
v  Velocity[y]           -0.38221         0.70133      0.00056238      0.00033828
v  Velocity[z]            -0.4201         0.51115      -0.0012391      -0.0013654
v  TurbEner             0.0010022        0.014595       0.0032848       0.0033447
v  Dissip              9.2133e-05        0.031047      0.00045228      0.00039097
v  TurbVisc               0.16335          11.362           4.711          5.2723
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              868:        0.89631E-01

===============================================================


 INSTANT    0.869000000E+03   TIME STEP NUMBER             869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997957E+04
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 :  0.23805E+00 0.12173E+01
   Friction velocity        uet   :  0.14239E-01 0.72545E-01
   Friction velocity        uk    :  0.17340E-01 0.38547E-01
   Dimensionless distance   yplus :  0.42548E+03 0.94365E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75624E+01      67   0.16797E-02   0.24781E-01 
c  VelocityX    0.46297E+04      12   0.73402E-02   0.40971E-03 
c  VelocityY    0.46297E+04      12   0.73402E-02   0.77501E-04 
c  VelocityZ    0.46297E+04      12   0.73402E-02   0.66886E-04 
c  TurbEner     0.59759E+01      13   0.80403E-04   0.14573E-08 
c  Dissip       0.14703E+01      15   0.85822E-03   0.95064E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.65           54514           26776           27270
v  Velocity[x]            0.29306          2.1276         0.90807         0.90984
v  Velocity[y]           -0.36763         0.70761      0.00055664       0.0003326
v  Velocity[z]           -0.42046          0.5042       -0.001241      -0.0013619
v  TurbEner             0.0010043        0.014559        0.003285       0.0033448
v  Dissip                9.21e-05        0.030477      0.00045217       0.0003909
v  TurbVisc               0.16314          11.343           4.711          5.2723
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              869:        0.90354E-01

===============================================================


 INSTANT    0.870000000E+03   TIME STEP NUMBER             870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001782E+04
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 :  0.23763E+00 0.13258E+01
   Friction velocity        uet   :  0.14214E-01 0.79012E-01
   Friction velocity        uk    :  0.17358E-01 0.38465E-01
   Dimensionless distance   yplus :  0.42637E+03 0.94336E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64901E+01      53   0.12570E-02   0.21285E-01 
c  VelocityX    0.46299E+04      12   0.63165E-02   0.35730E-03 
c  VelocityY    0.46299E+04      12   0.63165E-02   0.43021E-04 
c  VelocityZ    0.46299E+04      12   0.63165E-02   0.31839E-04 
c  TurbEner     0.59766E+01      13   0.77450E-04   0.13449E-08 
c  Dissip       0.14852E+01      14   0.54677E-03   0.76371E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.49           54522           26776           27270
v  Velocity[x]             0.2925          2.1744         0.90804         0.90982
v  Velocity[y]           -0.38243         0.70226      0.00055927       0.0003358
v  Velocity[z]           -0.42171         0.51173      -0.0012411      -0.0013643
v  TurbEner             0.0010013        0.014717       0.0032852       0.0033449
v  Dissip               9.207e-05        0.030576      0.00045223      0.00039093
v  TurbVisc               0.16362          11.339           4.711          5.2723
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              870:        0.89611E-01

===============================================================


 INSTANT    0.871000000E+03   TIME STEP NUMBER             871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000906E+04
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 :  0.23766E+00 0.12308E+01
   Friction velocity        uet   :  0.14217E-01 0.72301E-01
   Friction velocity        uk    :  0.17332E-01 0.38477E-01
   Dimensionless distance   yplus :  0.42603E+03 0.94332E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64670E+01      56   0.14849E-02   0.21205E-01 
c  VelocityX    0.46297E+04      12   0.68671E-02   0.37870E-03 
c  VelocityY    0.46297E+04      12   0.68671E-02   0.40042E-04 
c  VelocityZ    0.46297E+04      12   0.68671E-02   0.44536E-04 
c  TurbEner     0.59767E+01      13   0.12387E-03   0.15735E-08 
c  Dissip       0.14912E+01      16   0.17158E-02   0.30872E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.64           54532           26776           27270
v  Velocity[x]            0.29245          2.0051         0.90805         0.90982
v  Velocity[y]           -0.36615         0.70997      0.00055404      0.00033033
v  Velocity[z]           -0.42168         0.50639      -0.0012522      -0.0013773
v  TurbEner             0.0010047        0.015313       0.0032852       0.0033449
v  Dissip              9.2095e-05        0.031902      0.00045234      0.00039101
v  TurbVisc                0.1633          11.369          4.7111          5.2724
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              871:        0.89602E-01

===============================================================


 INSTANT    0.872000000E+03   TIME STEP NUMBER             872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001387E+04
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 :  0.23796E+00 0.13243E+01
   Friction velocity        uet   :  0.14234E-01 0.78930E-01
   Friction velocity        uk    :  0.17362E-01 0.38518E-01
   Dimensionless distance   yplus :  0.42599E+03 0.94297E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62124E+01      57   0.14217E-02   0.20362E-01 
c  VelocityX    0.46298E+04      12   0.70383E-02   0.35277E-03 
c  VelocityY    0.46298E+04      12   0.70383E-02   0.28274E-04 
c  VelocityZ    0.46298E+04      12   0.70383E-02   0.51330E-04 
c  TurbEner     0.59755E+01      13   0.11965E-03   0.16123E-08 
c  Dissip       0.14545E+01      17   0.21845E-02   0.70938E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.65           54540           26776           27270
v  Velocity[x]            0.29302          2.0854         0.90806         0.90983
v  Velocity[y]           -0.38238         0.69613      0.00054796      0.00032532
v  Velocity[z]           -0.41932         0.51085      -0.0012403      -0.0013658
v  TurbEner             0.0010061        0.014798        0.003285       0.0033447
v  Dissip              9.2048e-05         0.03055      0.00045204      0.00039079
v  TurbVisc               0.16332          11.347           4.711          5.2723
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              872:        0.89350E-01

===============================================================


 INSTANT    0.873000000E+03   TIME STEP NUMBER             873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000000E+04
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 :  0.23750E+00 0.12180E+01
   Friction velocity        uet   :  0.14207E-01 0.72583E-01
   Friction velocity        uk    :  0.17373E-01 0.38555E-01
   Dimensionless distance   yplus :  0.42673E+03 0.94284E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58928E+01      53   0.12997E-02   0.19322E-01 
c  VelocityX    0.46298E+04      12   0.64109E-02   0.32339E-03 
c  VelocityY    0.46298E+04      12   0.64109E-02   0.27471E-04 
c  VelocityZ    0.46298E+04      12   0.64109E-02   0.50439E-04 
c  TurbEner     0.59759E+01      12   0.63163E-04   0.55585E-09 
c  Dissip       0.14575E+01      14   0.56387E-03   0.37818E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.43           54548           26775           27270
v  Velocity[x]            0.29282          2.1367         0.90806         0.90983
v  Velocity[y]           -0.36791         0.70569      0.00054642      0.00032132
v  Velocity[z]            -0.4201         0.50401      -0.0012592      -0.0013814
v  TurbEner             0.0010034        0.014713        0.003285       0.0033447
v  Dissip              9.2056e-05        0.030183      0.00045194      0.00039072
v  TurbVisc               0.16368          11.349          4.7109          5.2722
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              873:        0.89257E-01

===============================================================


 INSTANT    0.874000000E+03   TIME STEP NUMBER             874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000447E+04
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 :  0.23786E+00 0.13233E+01
   Friction velocity        uet   :  0.14228E-01 0.78858E-01
   Friction velocity        uk    :  0.17350E-01 0.38552E-01
   Dimensionless distance   yplus :  0.42654E+03 0.94256E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65416E+01      55   0.15589E-02   0.21448E-01 
c  VelocityX    0.46298E+04      12   0.73086E-02   0.32672E-03 
c  VelocityY    0.46298E+04      12   0.73086E-02   0.68650E-04 
c  VelocityZ    0.46298E+04      12   0.73086E-02   0.11891E-03 
c  TurbEner     0.59769E+01      13   0.69491E-04   0.83079E-09 
c  Dissip       0.14756E+01      15   0.66255E-03   0.10770E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.55           54541           26776           27270
v  Velocity[x]            0.29251          2.1826         0.90805         0.90982
v  Velocity[y]           -0.38304         0.70063      0.00056129      0.00033858
v  Velocity[z]           -0.42204         0.51123       -0.001227      -0.0013515
v  TurbEner              0.001005        0.014821       0.0032851       0.0033448
v  Dissip              9.2073e-05        0.030305      0.00045202      0.00039075
v  TurbVisc               0.16339          11.318           4.711          5.2723
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              874:        0.89491E-01

===============================================================


 INSTANT    0.875000000E+03   TIME STEP NUMBER             875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998201E+04
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 :  0.23786E+00 0.12500E+01
   Friction velocity        uet   :  0.14227E-01 0.72816E-01
   Friction velocity        uk    :  0.17364E-01 0.38433E-01
   Dimensionless distance   yplus :  0.42598E+03 0.94207E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63384E+01      63   0.16665E-02   0.20782E-01 
c  VelocityX    0.46296E+04      12   0.64028E-02   0.45516E-03 
c  VelocityY    0.46296E+04      12   0.64028E-02   0.28077E-04 
c  VelocityZ    0.46296E+04      12   0.64028E-02   0.51096E-04 
c  TurbEner     0.59777E+01      13   0.12844E-03   0.17205E-08 
c  Dissip       0.14872E+01      16   0.19438E-02   0.42868E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.57           54515           26776           27270
v  Velocity[x]            0.29285           2.018         0.90805         0.90982
v  Velocity[y]           -0.36809          0.7084      0.00056136       0.0003389
v  Velocity[z]           -0.42141         0.50701      -0.0012336      -0.0013538
v  TurbEner             0.0010077        0.015443       0.0032854        0.003345
v  Dissip               9.207e-05        0.031807      0.00045223      0.00039092
v  TurbVisc               0.16318            11.3           4.711          5.2723
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              875:        0.90249E-01

===============================================================


 INSTANT    0.876000000E+03   TIME STEP NUMBER             876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998953E+04
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 :  0.23768E+00 0.13236E+01
   Friction velocity        uet   :  0.14216E-01 0.78883E-01
   Friction velocity        uk    :  0.17387E-01 0.38380E-01
   Dimensionless distance   yplus :  0.42709E+03 0.94159E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55728E+01      53   0.12396E-02   0.18282E-01 
c  VelocityX    0.46298E+04      12   0.60700E-02   0.31301E-03 
c  VelocityY    0.46298E+04      12   0.60700E-02   0.26839E-04 
c  VelocityZ    0.46298E+04      12   0.60700E-02   0.47884E-04 
c  TurbEner     0.59758E+01      14   0.12142E-03   0.20410E-08 
c  Dissip       0.14547E+01      16   0.20090E-02   0.62438E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.25           54523           26776           27271
v  Velocity[x]            0.29248          2.0916         0.90805         0.90982
v  Velocity[y]           -0.38272         0.70025       0.0005537      0.00033166
v  Velocity[z]           -0.42138         0.51384      -0.0012366       -0.001359
v  TurbEner             0.0010044        0.014919       0.0032853       0.0033449
v  Dissip              9.2061e-05        0.030557        0.000452      0.00039075
v  TurbVisc                0.1638          11.336          4.7111          5.2724
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              876:        0.89091E-01

===============================================================


 INSTANT    0.877000000E+03   TIME STEP NUMBER             877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000311E+04
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 :  0.23783E+00 0.12172E+01
   Friction velocity        uet   :  0.14225E-01 0.72539E-01
   Friction velocity        uk    :  0.17359E-01 0.38437E-01
   Dimensionless distance   yplus :  0.42672E+03 0.94106E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58966E+01      56   0.12316E-02   0.19325E-01 
c  VelocityX    0.46298E+04      12   0.66773E-02   0.30900E-03 
c  VelocityY    0.46298E+04      12   0.66773E-02   0.24273E-04 
c  VelocityZ    0.46298E+04      12   0.66773E-02   0.46318E-04 
c  TurbEner     0.59759E+01      12   0.61623E-04   0.58077E-09 
c  Dissip       0.14605E+01      14   0.47271E-03   0.34295E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -175.8           54532           26776           27270
v  Velocity[x]            0.29271           2.142         0.90805         0.90982
v  Velocity[y]           -0.36646         0.70645      0.00055528      0.00032958
v  Velocity[z]            -0.4216         0.50792      -0.0012478      -0.0013681
v  TurbEner             0.0010074        0.014827       0.0032852       0.0033448
v  Dissip              9.2021e-05        0.030292      0.00045196      0.00039071
v  TurbVisc                0.1635          11.326          4.7111          5.2724
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              877:        0.89434E-01

===============================================================


 INSTANT    0.878000000E+03   TIME STEP NUMBER             878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001681E+04
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 :  0.23783E+00 0.13252E+01
   Friction velocity        uet   :  0.14225E-01 0.78966E-01
   Friction velocity        uk    :  0.17385E-01 0.38503E-01
   Dimensionless distance   yplus :  0.42656E+03 0.94115E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63736E+01      56   0.12572E-02   0.20889E-01 
c  VelocityX    0.46298E+04      12   0.70042E-02   0.36678E-03 
c  VelocityY    0.46298E+04      12   0.70042E-02   0.36951E-04 
c  VelocityZ    0.46298E+04      12   0.70042E-02   0.88122E-04 
c  TurbEner     0.59769E+01      12   0.67565E-04   0.73643E-09 
c  Dissip       0.14814E+01      15   0.72517E-03   0.12421E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.7           54542           26776           27270
v  Velocity[x]            0.29303          2.1824         0.90806         0.90984
v  Velocity[y]           -0.38267          0.6997      0.00055698      0.00033227
v  Velocity[z]           -0.41927         0.51209      -0.0012267      -0.0013508
v  TurbEner             0.0010084        0.014925       0.0032854       0.0033449
v  Dissip              9.2028e-05         0.03053       0.0004521       0.0003908
v  TurbVisc               0.16352          11.327          4.7111          5.2724
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              878:        0.89210E-01

===============================================================


 INSTANT    0.879000000E+03   TIME STEP NUMBER             879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998576E+04
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 :  0.23753E+00 0.12252E+01
   Friction velocity        uet   :  0.14206E-01 0.72323E-01
   Friction velocity        uk    :  0.17394E-01 0.38458E-01
   Dimensionless distance   yplus :  0.42717E+03 0.94110E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55791E+01      56   0.13623E-02   0.18297E-01 
c  VelocityX    0.46298E+04      12   0.68427E-02   0.35588E-03 
c  VelocityY    0.46298E+04      12   0.68427E-02   0.27980E-04 
c  VelocityZ    0.46298E+04      12   0.68427E-02   0.39961E-04 
c  TurbEner     0.59774E+01      13   0.12571E-03   0.13917E-08 
c  Dissip       0.14981E+01      16   0.20816E-02   0.49163E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.59           54548           26776           27270
v  Velocity[x]            0.29263           2.018         0.90806         0.90983
v  Velocity[y]           -0.36813         0.70801      0.00055229      0.00032637
v  Velocity[z]           -0.42021         0.50491      -0.0012504      -0.0013725
v  TurbEner              0.001007        0.015524       0.0032855        0.003345
v  Dissip              9.2014e-05        0.032155      0.00045236      0.00039099
v  TurbVisc               0.16392           11.36          4.7113          5.2725
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              879:        0.89602E-01

===============================================================


 INSTANT    0.880000000E+03   TIME STEP NUMBER             880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000483E+04
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 :  0.23790E+00 0.13247E+01
   Friction velocity        uet   :  0.14228E-01 0.78953E-01
   Friction velocity        uk    :  0.17381E-01 0.38475E-01
   Dimensionless distance   yplus :  0.42725E+03 0.94200E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64844E+01      56   0.15992E-02   0.21252E-01 
c  VelocityX    0.46298E+04      12   0.74167E-02   0.39596E-03 
c  VelocityY    0.46298E+04      12   0.74167E-02   0.25038E-04 
c  VelocityZ    0.46298E+04      12   0.74167E-02   0.52481E-04 
c  TurbEner     0.59764E+01      14   0.13116E-03   0.18711E-08 
c  Dissip       0.14672E+01      16   0.20418E-02   0.63498E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.6           54541           26776           27270
v  Velocity[x]            0.29272          2.0904         0.90807         0.90985
v  Velocity[y]           -0.38254         0.69931      0.00055503      0.00033347
v  Velocity[z]           -0.42255         0.51228      -0.0012451      -0.0013703
v  TurbEner             0.0010094        0.014948       0.0032855        0.003345
v  Dissip              9.2038e-05        0.030866      0.00045219      0.00039087
v  TurbVisc               0.16396          11.343          4.7113          5.2725
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              880:        0.89211E-01

===============================================================


 INSTANT    0.881000000E+03   TIME STEP NUMBER             881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998768E+04
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 :  0.23769E+00 0.12159E+01
   Friction velocity        uet   :  0.14216E-01 0.72463E-01
   Friction velocity        uk    :  0.17402E-01 0.38497E-01
   Dimensionless distance   yplus :  0.42693E+03 0.94305E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65489E+01      55   0.15532E-02   0.21467E-01 
c  VelocityX    0.46299E+04      12   0.69949E-02   0.43318E-03 
c  VelocityY    0.46299E+04      12   0.69949E-02   0.30602E-04 
c  VelocityZ    0.46299E+04      12   0.69949E-02   0.59144E-04 
c  TurbEner     0.59767E+01      13   0.80224E-04   0.11037E-08 
c  Dissip       0.14693E+01      14   0.58047E-03   0.48205E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.18           54515           26776           27270
v  Velocity[x]            0.29273          2.1408         0.90807         0.90984
v  Velocity[y]           -0.36619         0.70586      0.00055478      0.00033332
v  Velocity[z]           -0.42028         0.50686      -0.0012418      -0.0013625
v  TurbEner             0.0010131        0.014804       0.0032856       0.0033451
v  Dissip               9.201e-05        0.030507      0.00045216      0.00039085
v  TurbVisc                0.1639          11.335          4.7113          5.2725
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              881:        0.88488E-01

===============================================================


 INSTANT    0.882000000E+03   TIME STEP NUMBER             882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000547E+04
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 :  0.23798E+00 0.13251E+01
   Friction velocity        uet   :  0.14232E-01 0.78973E-01
   Friction velocity        uk    :  0.17433E-01 0.38452E-01
   Dimensionless distance   yplus :  0.42822E+03 0.94349E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63106E+01      57   0.13767E-02   0.20691E-01 
c  VelocityX    0.46299E+04      12   0.70284E-02   0.36433E-03 
c  VelocityY    0.46299E+04      12   0.70284E-02   0.67612E-04 
c  VelocityZ    0.46299E+04      12   0.70284E-02   0.10577E-03 
c  TurbEner     0.59773E+01      13   0.82773E-04   0.13104E-08 
c  Dissip       0.14907E+01      15   0.67962E-03   0.11451E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.21           54524           26777           27271
v  Velocity[x]            0.29279          2.1834         0.90805         0.90983
v  Velocity[y]            -0.3825         0.70134       0.0005608      0.00033812
v  Velocity[z]           -0.42116         0.51113      -0.0012278      -0.0013533
v  TurbEner             0.0010106        0.014898       0.0032858       0.0033452
v  Dissip              9.2062e-05        0.030717      0.00045231      0.00039095
v  TurbVisc               0.16468           11.37          4.7114          5.2726
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              882:        0.89486E-01

===============================================================


 INSTANT    0.883000000E+03   TIME STEP NUMBER             883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998289E+04
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 :  0.23767E+00 0.12128E+01
   Friction velocity        uet   :  0.14214E-01 0.72289E-01
   Friction velocity        uk    :  0.17412E-01 0.38536E-01
   Dimensionless distance   yplus :  0.42803E+03 0.94383E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58773E+01      58   0.12981E-02   0.19272E-01 
c  VelocityX    0.46297E+04      12   0.64004E-02   0.39928E-03 
c  VelocityY    0.46297E+04      12   0.64004E-02   0.20687E-04 
c  VelocityZ    0.46297E+04      12   0.64004E-02   0.45568E-04 
c  TurbEner     0.59779E+01      13   0.12658E-03   0.15298E-08 
c  Dissip       0.15052E+01      16   0.19774E-02   0.45187E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.95           54533           26777           27271
v  Velocity[x]            0.29283          2.0157         0.90805         0.90982
v  Velocity[y]           -0.36808         0.70875       0.0005573      0.00033183
v  Velocity[z]           -0.42222         0.50413      -0.0012471      -0.0013693
v  TurbEner             0.0010148        0.015493        0.003286       0.0033453
v  Dissip              9.2037e-05        0.032248      0.00045246      0.00039105
v  TurbVisc               0.16455           11.34          4.7115          5.2727
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              883:        0.89537E-01

===============================================================


 INSTANT    0.884000000E+03   TIME STEP NUMBER             884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998464E+04
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 :  0.23770E+00 0.13247E+01
   Friction velocity        uet   :  0.14216E-01 0.78958E-01
   Friction velocity        uk    :  0.17448E-01 0.38561E-01
   Dimensionless distance   yplus :  0.42808E+03 0.94374E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55785E+01      60   0.12732E-02   0.18283E-01 
c  VelocityX    0.46298E+04      12   0.64921E-02   0.30729E-03 
c  VelocityY    0.46298E+04      12   0.64921E-02   0.24307E-04 
c  VelocityZ    0.46298E+04      12   0.64921E-02   0.44000E-04 
c  TurbEner     0.59766E+01      13   0.13779E-03   0.19271E-08 
c  Dissip       0.14678E+01      16   0.22190E-02   0.73373E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.25           54542           26777           27271
v  Velocity[x]            0.29275          2.0891         0.90804         0.90982
v  Velocity[y]           -0.38287         0.69761        0.000558      0.00033433
v  Velocity[z]           -0.41957         0.51153       -0.001235      -0.0013609
v  TurbEner             0.0010168        0.014886       0.0032859       0.0033453
v  Dissip              9.2024e-05         0.03084      0.00045218      0.00039086
v  TurbVisc               0.16468          11.339          4.7116          5.2728
v  total_pressure           83078      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              884:        0.89709E-01

===============================================================


 INSTANT    0.885000000E+03   TIME STEP NUMBER             885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998449E+04
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 :  0.23742E+00 0.12179E+01
   Friction velocity        uet   :  0.14199E-01 0.72585E-01
   Friction velocity        uk    :  0.17465E-01 0.38554E-01
   Dimensionless distance   yplus :  0.42891E+03 0.94388E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56969E+01      57   0.12020E-02   0.18693E-01 
c  VelocityX    0.46299E+04      12   0.67653E-02   0.29362E-03 
c  VelocityY    0.46299E+04      12   0.67653E-02   0.24903E-04 
c  VelocityZ    0.46299E+04      12   0.67653E-02   0.49885E-04 
c  TurbEner     0.59768E+01      12   0.63471E-04   0.56673E-09 
c  Dissip       0.14699E+01      13   0.56881E-03   0.39956E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -173.96           54551           26777           27272
v  Velocity[x]            0.29255          2.1416         0.90806         0.90983
v  Velocity[y]           -0.36798         0.70553      0.00055149      0.00032503
v  Velocity[z]           -0.42006         0.50706      -0.0012505      -0.0013737
v  TurbEner             0.0010155         0.01474       0.0032859       0.0033454
v  Dissip              9.1998e-05        0.030472      0.00045211      0.00039082
v  TurbVisc               0.16519          11.368          4.7117          5.2729
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              885:        0.89904E-01

===============================================================


 INSTANT    0.886000000E+03   TIME STEP NUMBER             886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999975E+04
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 :  0.23788E+00 0.13243E+01
   Friction velocity        uet   :  0.14227E-01 0.78920E-01
   Friction velocity        uk    :  0.17454E-01 0.38414E-01
   Dimensionless distance   yplus :  0.42902E+03 0.94386E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.79219E+01      61   0.16943E-02   0.25956E-01 
c  VelocityX    0.46299E+04      12   0.76449E-02   0.39399E-03 
c  VelocityY    0.46299E+04      12   0.76449E-02   0.49056E-04 
c  VelocityZ    0.46299E+04      12   0.76449E-02   0.98295E-04 
c  TurbEner     0.59778E+01      13   0.67166E-04   0.80197E-09 
c  Dissip       0.14905E+01      15   0.67312E-03   0.11135E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.01           54543           26778           27272
v  Velocity[x]            0.29275           2.187         0.90805         0.90983
v  Velocity[y]           -0.38287         0.69922      0.00056509      0.00034075
v  Velocity[z]           -0.42083         0.51389      -0.0012275      -0.0013544
v  TurbEner             0.0010177        0.014811       0.0032859       0.0033454
v  Dissip              9.1994e-05         0.03061      0.00045221      0.00039088
v  TurbVisc                0.1652          11.348          4.7118           5.273
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              886:        0.90654E-01

===============================================================


 INSTANT    0.887000000E+03   TIME STEP NUMBER             887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999853E+04
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 :  0.23796E+00 0.12170E+01
   Friction velocity        uet   :  0.14231E-01 0.72529E-01
   Friction velocity        uk    :  0.17473E-01 0.38511E-01
   Dimensionless distance   yplus :  0.42862E+03 0.94384E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.75047E+01      71   0.17531E-02   0.24614E-01 
c  VelocityX    0.46298E+04      12   0.66582E-02   0.48759E-03 
c  VelocityY    0.46298E+04      12   0.66582E-02   0.63995E-04 
c  VelocityZ    0.46298E+04      12   0.66582E-02   0.61270E-04 
c  TurbEner     0.59783E+01      13   0.13850E-03   0.19892E-08 
c  Dissip       0.14959E+01      16   0.19555E-02   0.41411E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.56           54516           26777           27271
v  Velocity[x]            0.29303          2.0051         0.90807         0.90984
v  Velocity[y]           -0.36655         0.70723      0.00056503      0.00033884
v  Velocity[z]           -0.42047         0.50796      -0.0012419      -0.0013631
v  TurbEner             0.0010199        0.015475       0.0032862       0.0033457
v  Dissip              9.2002e-05        0.032134       0.0004524      0.00039104
v  TurbVisc               0.16506          11.344          4.7118           5.273
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              887:        0.91898E-01

===============================================================


 INSTANT    0.888000000E+03   TIME STEP NUMBER             888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000883E+04
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 :  0.23771E+00 0.13238E+01
   Friction velocity        uet   :  0.14216E-01 0.78892E-01
   Friction velocity        uk    :  0.17492E-01 0.38571E-01
   Dimensionless distance   yplus :  0.42963E+03 0.94343E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60816E+01      53   0.12885E-02   0.19946E-01 
c  VelocityX    0.46299E+04      12   0.65739E-02   0.34867E-03 
c  VelocityY    0.46299E+04      12   0.65739E-02   0.35522E-04 
c  VelocityZ    0.46299E+04      12   0.65739E-02   0.32338E-04 
c  TurbEner     0.59769E+01      14   0.14371E-03   0.22699E-08 
c  Dissip       0.14616E+01      17   0.23563E-02   0.74450E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.73           54525           26777           27271
v  Velocity[x]             0.2926          2.1007         0.90804         0.90981
v  Velocity[y]            -0.3827         0.69988      0.00055774      0.00033514
v  Velocity[z]            -0.4221         0.51206      -0.0012424       -0.001365
v  TurbEner             0.0010161        0.014802       0.0032862       0.0033457
v  Dissip              9.2047e-05        0.030539      0.00045215      0.00039087
v  TurbVisc               0.16565          11.319          4.7119          5.2731
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              888:        0.89559E-01

===============================================================


 INSTANT    0.889000000E+03   TIME STEP NUMBER             889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999737E+04
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 :  0.23764E+00 0.12166E+01
   Friction velocity        uet   :  0.14212E-01 0.72507E-01
   Friction velocity        uk    :  0.17459E-01 0.38495E-01
   Dimensionless distance   yplus :  0.42922E+03 0.94376E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62296E+01      51   0.12542E-02   0.20424E-01 
c  VelocityX    0.46298E+04      12   0.66737E-02   0.29172E-03 
c  VelocityY    0.46298E+04      12   0.66737E-02   0.34435E-04 
c  VelocityZ    0.46298E+04      12   0.66737E-02   0.40345E-04 
c  TurbEner     0.59768E+01      13   0.59926E-04   0.75523E-09 
c  Dissip       0.14647E+01      13   0.32600E-03   0.21745E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.63           54535           26777           27271
v  Velocity[x]            0.29279          2.1402         0.90805         0.90982
v  Velocity[y]           -0.36822           0.708      0.00054939      0.00032251
v  Velocity[z]           -0.42126         0.50489      -0.0012486      -0.0013698
v  TurbEner             0.0010184        0.014775       0.0032861       0.0033456
v  Dissip              9.2075e-05         0.03038      0.00045207      0.00039081
v  TurbVisc               0.16536          11.326           4.712          5.2732
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              889:        0.88440E-01

===============================================================


 INSTANT    0.890000000E+03   TIME STEP NUMBER             890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999822E+04
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 :  0.23796E+00 0.13238E+01
   Friction velocity        uet   :  0.14231E-01 0.78890E-01
   Friction velocity        uk    :  0.17479E-01 0.38477E-01
   Dimensionless distance   yplus :  0.42901E+03 0.94388E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61296E+01      59   0.12838E-02   0.20092E-01 
c  VelocityX    0.46299E+04      12   0.71493E-02   0.28885E-03 
c  VelocityY    0.46299E+04      12   0.71493E-02   0.27261E-04 
c  VelocityZ    0.46299E+04      12   0.71493E-02   0.74406E-04 
c  TurbEner     0.59780E+01      12   0.69363E-04   0.71157E-09 
c  Dissip       0.14887E+01      15   0.75939E-03   0.13087E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.62           54542           26778           27272
v  Velocity[x]            0.29294          2.1831         0.90804         0.90982
v  Velocity[y]           -0.38258         0.70105      0.00055906      0.00033334
v  Velocity[z]           -0.41971         0.51232      -0.0012342      -0.0013592
v  TurbEner             0.0010185          0.0149       0.0032862       0.0033457
v  Dissip              9.2053e-05        0.030674      0.00045223      0.00039091
v  TurbVisc               0.16532          11.364          4.7119          5.2731
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              890:        0.89646E-01

===============================================================


 INSTANT    0.891000000E+03   TIME STEP NUMBER             891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998356E+04
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 :  0.23730E+00 0.12172E+01
   Friction velocity        uet   :  0.14192E-01 0.72546E-01
   Friction velocity        uk    :  0.17480E-01 0.38537E-01
   Dimensionless distance   yplus :  0.42952E+03 0.94349E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66219E+01      55   0.14565E-02   0.21717E-01 
c  VelocityX    0.46299E+04      12   0.66655E-02   0.41435E-03 
c  VelocityY    0.46299E+04      12   0.66655E-02   0.29217E-04 
c  VelocityZ    0.46299E+04      12   0.66655E-02   0.60684E-04 
c  TurbEner     0.59781E+01      13   0.12359E-03   0.12745E-08 
c  Dissip       0.14975E+01      16   0.19763E-02   0.42041E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.95           54551           26778           27272
v  Velocity[x]            0.29227          2.0063         0.90805         0.90982
v  Velocity[y]            -0.3667         0.70744      0.00055697      0.00032977
v  Velocity[z]           -0.41946         0.50631      -0.0012568      -0.0013824
v  TurbEner             0.0010153        0.015533       0.0032863       0.0033458
v  Dissip              9.2061e-05        0.032227      0.00045241      0.00039105
v  TurbVisc               0.16565          11.348           4.712          5.2732
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              891:        0.89351E-01

===============================================================


 INSTANT    0.892000000E+03   TIME STEP NUMBER             892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000140E+04
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 :  0.23803E+00 0.13249E+01
   Friction velocity        uet   :  0.14235E-01 0.78960E-01
   Friction velocity        uk    :  0.17452E-01 0.38574E-01
   Dimensionless distance   yplus :  0.42925E+03 0.94386E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66831E+01      55   0.15998E-02   0.21903E-01 
c  VelocityX    0.46299E+04      12   0.72647E-02   0.36057E-03 
c  VelocityY    0.46299E+04      12   0.72647E-02   0.38562E-04 
c  VelocityZ    0.46299E+04      12   0.72647E-02   0.33292E-04 
c  TurbEner     0.59770E+01      14   0.15770E-03   0.22063E-08 
c  Dissip       0.14570E+01      17   0.26192E-02   0.85655E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.41           54542           26778           27272
v  Velocity[x]            0.29274          2.0974         0.90806         0.90984
v  Velocity[y]           -0.38223          0.7001      0.00055511      0.00033446
v  Velocity[z]           -0.42151         0.51139      -0.0012399      -0.0013623
v  TurbEner             0.0010161        0.014758       0.0032861       0.0033457
v  Dissip              9.2065e-05        0.030399      0.00045211      0.00039084
v  TurbVisc               0.16547          11.356           4.712          5.2732
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              892:        0.89507E-01

===============================================================


 INSTANT    0.893000000E+03   TIME STEP NUMBER             893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000921E+04
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 :  0.23790E+00 0.12137E+01
   Friction velocity        uet   :  0.14227E-01 0.72334E-01
   Friction velocity        uk    :  0.17459E-01 0.38616E-01
   Dimensionless distance   yplus :  0.42853E+03 0.94388E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72494E+01      61   0.16000E-02   0.23764E-01 
c  VelocityX    0.46299E+04      12   0.71040E-02   0.46110E-03 
c  VelocityY    0.46299E+04      12   0.71040E-02   0.45780E-04 
c  VelocityZ    0.46299E+04      12   0.71040E-02   0.41755E-04 
c  TurbEner     0.59773E+01      13   0.63462E-04   0.98181E-09 
c  Dissip       0.14569E+01      14   0.42930E-03   0.32280E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.43           54515           26777           27271
v  Velocity[x]            0.29331          2.1369         0.90807         0.90984
v  Velocity[y]           -0.36711         0.70841      0.00056187      0.00034007
v  Velocity[z]           -0.42221         0.50486      -0.0012448      -0.0013665
v  TurbEner             0.0010178        0.014708       0.0032862       0.0033457
v  Dissip              9.2081e-05        0.030136      0.00045203      0.00039079
v  TurbVisc               0.16519          11.334          4.7121          5.2733
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              893:        0.90079E-01

===============================================================


 INSTANT    0.894000000E+03   TIME STEP NUMBER             894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001869E+04
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 :  0.23751E+00 0.13254E+01
   Friction velocity        uet   :  0.14204E-01 0.78992E-01
   Friction velocity        uk    :  0.17474E-01 0.38574E-01
   Dimensionless distance   yplus :  0.42940E+03 0.94370E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58398E+01      56   0.12322E-02   0.19159E-01 
c  VelocityX    0.46300E+04      12   0.74040E-02   0.32952E-03 
c  VelocityY    0.46300E+04      12   0.74040E-02   0.30925E-04 
c  VelocityZ    0.46300E+04      12   0.74040E-02   0.30096E-04 
c  TurbEner     0.59776E+01      13   0.73150E-04   0.11475E-08 
c  Dissip       0.14769E+01      15   0.70723E-03   0.11902E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.45           54525           26777           27271
v  Velocity[x]            0.29264            2.18         0.90805         0.90983
v  Velocity[y]           -0.38236         0.69794      0.00055403      0.00033114
v  Velocity[z]           -0.42092         0.51197      -0.0012387      -0.0013611
v  TurbEner             0.0010137        0.014824       0.0032863       0.0033457
v  Dissip              9.2087e-05        0.030381      0.00045215      0.00039087
v  TurbVisc               0.16573          11.328          4.7121          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              894:        0.89988E-01

===============================================================


 INSTANT    0.895000000E+03   TIME STEP NUMBER             895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001666E+04
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 :  0.23812E+00 0.12231E+01
   Friction velocity        uet   :  0.14240E-01 0.72569E-01
   Friction velocity        uk    :  0.17438E-01 0.38486E-01
   Dimensionless distance   yplus :  0.42883E+03 0.94425E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64275E+01      59   0.14521E-02   0.21068E-01 
c  VelocityX    0.46299E+04      12   0.71996E-02   0.38394E-03 
c  VelocityY    0.46299E+04      12   0.71996E-02   0.29593E-04 
c  VelocityZ    0.46299E+04      12   0.71996E-02   0.31081E-04 
c  TurbEner     0.59776E+01      13   0.11727E-03   0.12785E-08 
c  Dissip       0.14879E+01      16   0.19248E-02   0.40071E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.99           54534           26776           27270
v  Velocity[x]            0.29265          2.0119         0.90804         0.90981
v  Velocity[y]           -0.36685         0.70602      0.00054984      0.00032516
v  Velocity[z]            -0.4223          0.5058       -0.001253      -0.0013738
v  TurbEner             0.0010158        0.015402       0.0032863       0.0033457
v  Dissip              9.2051e-05        0.031887      0.00045227      0.00039095
v  TurbVisc               0.16539           11.36          4.7121          5.2734
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              895:        0.90390E-01

===============================================================


 INSTANT    0.896000000E+03   TIME STEP NUMBER             896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002636E+04
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 :  0.23776E+00 0.13242E+01
   Friction velocity        uet   :  0.14218E-01 0.78920E-01
   Friction velocity        uk    :  0.17457E-01 0.38505E-01
   Dimensionless distance   yplus :  0.42849E+03 0.94403E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65158E+01      59   0.13158E-02   0.21357E-01 
c  VelocityX    0.46299E+04      12   0.69478E-02   0.39945E-03 
c  VelocityY    0.46299E+04      12   0.69478E-02   0.28632E-04 
c  VelocityZ    0.46299E+04      12   0.69478E-02   0.61308E-04 
c  TurbEner     0.59765E+01      13   0.13022E-03   0.17169E-08 
c  Dissip       0.14595E+01      16   0.19959E-02   0.60018E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.18           54542           26776           27270
v  Velocity[x]            0.29286          2.0903         0.90805         0.90983
v  Velocity[y]           -0.38283         0.70092      0.00054629      0.00032381
v  Velocity[z]           -0.41867          0.5105      -0.0012435      -0.0013677
v  TurbEner             0.0010157        0.014873       0.0032861       0.0033456
v  Dissip              9.2039e-05        0.030634      0.00045203      0.00039078
v  TurbVisc               0.16528          11.345          4.7121          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              896:        0.89610E-01

===============================================================


 INSTANT    0.897000000E+03   TIME STEP NUMBER             897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000047E+04
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 :  0.23766E+00 0.12136E+01
   Friction velocity        uet   :  0.14213E-01 0.72330E-01
   Friction velocity        uk    :  0.17456E-01 0.38569E-01
   Dimensionless distance   yplus :  0.42882E+03 0.94399E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67607E+01      55   0.13945E-02   0.22160E-01 
c  VelocityX    0.46299E+04      13   0.63116E-02   0.32637E-03 
c  VelocityY    0.46299E+04      13   0.63116E-02   0.27468E-04 
c  VelocityZ    0.46299E+04      13   0.63116E-02   0.98540E-04 
c  TurbEner     0.59769E+01      12   0.74323E-04   0.71575E-09 
c  Dissip       0.14623E+01      14   0.69843E-03   0.54640E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -178           54548           26775           27269
v  Velocity[x]            0.29285          2.1492         0.90806         0.90983
v  Velocity[y]           -0.36737         0.70977      0.00055645      0.00032997
v  Velocity[z]           -0.42085          0.5044      -0.0012478        -0.00137
v  TurbEner             0.0010132        0.014727       0.0032861       0.0033456
v  Dissip              9.2072e-05        0.030165        0.000452      0.00039075
v  TurbVisc               0.16552          11.349          4.7122          5.2734
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              897:        0.90028E-01

===============================================================


 INSTANT    0.898000000E+03   TIME STEP NUMBER             898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001500E+04
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 :  0.23771E+00 0.13249E+01
   Friction velocity        uet   :  0.14216E-01 0.78960E-01
   Friction velocity        uk    :  0.17434E-01 0.38620E-01
   Dimensionless distance   yplus :  0.42867E+03 0.94431E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57157E+01      61   0.14938E-02   0.18753E-01 
c  VelocityX    0.46299E+04      12   0.70445E-02   0.27320E-03 
c  VelocityY    0.46299E+04      12   0.70445E-02   0.40579E-04 
c  VelocityZ    0.46299E+04      12   0.70445E-02   0.47537E-04 
c  TurbEner     0.59778E+01      13   0.75999E-04   0.94861E-09 
c  Dissip       0.14784E+01      15   0.73408E-03   0.11215E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.86           54541           26776           27270
v  Velocity[x]            0.29255          2.1787         0.90806         0.90984
v  Velocity[y]            -0.3822         0.69718      0.00055774       0.0003355
v  Velocity[z]           -0.42203         0.51194       -0.001237      -0.0013619
v  TurbEner             0.0010146        0.014905       0.0032864       0.0033457
v  Dissip              9.2104e-05        0.030528      0.00045213      0.00039083
v  TurbVisc               0.16538          11.328          4.7122          5.2735
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              898:        0.90357E-01

===============================================================


 INSTANT    0.899000000E+03   TIME STEP NUMBER             899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997635E+04
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 :  0.23778E+00 0.12298E+01
   Friction velocity        uet   :  0.14219E-01 0.72611E-01
   Friction velocity        uk    :  0.17447E-01 0.38549E-01
   Dimensionless distance   yplus :  0.42813E+03 0.94432E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63762E+01      58   0.14734E-02   0.20892E-01 
c  VelocityX    0.46299E+04      12   0.76152E-02   0.37672E-03 
c  VelocityY    0.46299E+04      12   0.76152E-02   0.38521E-04 
c  VelocityZ    0.46299E+04      12   0.76152E-02   0.41779E-04 
c  TurbEner     0.59790E+01      13   0.79885E-04   0.11570E-08 
c  Dissip       0.15099E+01      15   0.10584E-02   0.20730E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.34           54515           26776           27270
v  Velocity[x]            0.29278          2.2082         0.90806         0.90983
v  Velocity[y]            -0.3661         0.70708      0.00057212      0.00034838
v  Velocity[z]           -0.42069         0.50652      -0.0012336      -0.0013567
v  TurbEner             0.0010171         0.01513       0.0032865       0.0033458
v  Dissip               9.208e-05        0.031187      0.00045238        0.000391
v  TurbVisc               0.16516          11.322          4.7123          5.2735
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              899:        0.89505E-01

===============================================================


 INSTANT    0.900000000E+03   TIME STEP NUMBER             900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000347E+04
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 :  0.23779E+00 0.13242E+01
   Friction velocity        uet   :  0.14220E-01 0.78907E-01
   Friction velocity        uk    :  0.17468E-01 0.38565E-01
   Dimensionless distance   yplus :  0.42916E+03 0.94456E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63871E+01      57   0.16015E-02   0.20957E-01 
c  VelocityX    0.46299E+04      12   0.69807E-02   0.48798E-03 
c  VelocityY    0.46299E+04      12   0.69807E-02   0.24241E-04 
c  VelocityZ    0.46299E+04      12   0.69807E-02   0.35843E-04 
c  TurbEner     0.59790E+01      13   0.12419E-03   0.15724E-08 
c  Dissip       0.15356E+01      16   0.23997E-02   0.67777E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.51           54522           26777           27271
v  Velocity[x]            0.29267          2.0368         0.90806         0.90983
v  Velocity[y]           -0.38226         0.70096        0.000564      0.00034007
v  Velocity[z]           -0.42131         0.51112      -0.0012504      -0.0013731
v  TurbEner             0.0010135        0.015749       0.0032867       0.0033459
v  Dissip              9.2078e-05        0.033102       0.0004527      0.00039124
v  TurbVisc               0.16575          11.353          4.7123          5.2735
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              900:        0.89897E-01

===============================================================


 INSTANT    0.901000000E+03   TIME STEP NUMBER             901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998965E+04
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 :  0.23793E+00 0.12181E+01
   Friction velocity        uet   :  0.14229E-01 0.72597E-01
   Friction velocity        uk    :  0.17437E-01 0.38483E-01
   Dimensionless distance   yplus :  0.42874E+03 0.94526E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61410E+01      58   0.13958E-02   0.20124E-01 
c  VelocityX    0.46299E+04      13   0.66993E-02   0.39282E-03 
c  VelocityY    0.46299E+04      13   0.66993E-02   0.35837E-04 
c  VelocityZ    0.46299E+04      13   0.66993E-02   0.10420E-03 
c  TurbEner     0.59775E+01      14   0.14043E-03   0.21962E-08 
c  Dissip       0.15111E+01      16   0.17837E-02   0.51665E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.24           54523           26776           27270
v  Velocity[x]            0.29264          2.1078         0.90804         0.90982
v  Velocity[y]           -0.36771         0.70935      0.00056806      0.00034427
v  Velocity[z]           -0.42147         0.50415      -0.0012395      -0.0013648
v  TurbEner             0.0010168         0.01515       0.0032864       0.0033457
v  Dissip              9.2029e-05        0.031987      0.00045252      0.00039111
v  TurbVisc               0.16545          11.336          4.7124          5.2735
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              901:        0.90659E-01

===============================================================


 INSTANT    0.902000000E+03   TIME STEP NUMBER             902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001824E+04
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 :  0.23792E+00 0.13237E+01
   Friction velocity        uet   :  0.14228E-01 0.78882E-01
   Friction velocity        uk    :  0.17465E-01 0.38543E-01
   Dimensionless distance   yplus :  0.42859E+03 0.94532E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56365E+01      58   0.12902E-02   0.18491E-01 
c  VelocityX    0.46299E+04      12   0.57887E-02   0.34609E-03 
c  VelocityY    0.46299E+04      12   0.57887E-02   0.28490E-04 
c  VelocityZ    0.46299E+04      12   0.57887E-02   0.42921E-04 
c  TurbEner     0.59776E+01      12   0.62777E-04   0.64434E-09 
c  Dissip       0.15280E+01      14   0.44621E-03   0.53133E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.52           54508           26777           27271
v  Velocity[x]            0.29304          2.1564         0.90805         0.90983
v  Velocity[y]           -0.38235         0.70173      0.00056875      0.00034628
v  Velocity[z]           -0.41903         0.51181      -0.0012265      -0.0013509
v  TurbEner             0.0010178        0.015039       0.0032864       0.0033457
v  Dissip              9.2034e-05        0.032009      0.00045262      0.00039118
v  TurbVisc               0.16543          11.341          4.7123          5.2735
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              902:        0.89645E-01

===============================================================


 INSTANT    0.903000000E+03   TIME STEP NUMBER             903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998212E+04
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 :  0.23733E+00 0.12179E+01
   Friction velocity        uet   :  0.14193E-01 0.72583E-01
   Friction velocity        uk    :  0.17474E-01 0.38612E-01
   Dimensionless distance   yplus :  0.42923E+03 0.94522E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54750E+01      52   0.11464E-02   0.17947E-01 
c  VelocityX    0.46299E+04      12   0.68114E-02   0.29496E-03 
c  VelocityY    0.46299E+04      12   0.68114E-02   0.21700E-04 
c  VelocityZ    0.46299E+04      12   0.68114E-02   0.31512E-04 
c  TurbEner     0.59775E+01      13   0.70963E-04   0.10906E-08 
c  Dissip       0.15550E+01      15   0.95477E-03   0.21962E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.92           54515           26776           27270
v  Velocity[x]            0.29281          2.1928         0.90805         0.90982
v  Velocity[y]           -0.36654         0.70787       0.0005624      0.00033654
v  Velocity[z]           -0.42135         0.50601      -0.0012322      -0.0013542
v  TurbEner             0.0010159        0.015062       0.0032862       0.0033456
v  Dissip              9.2049e-05        0.032378       0.0004528      0.00039129
v  TurbVisc                0.1658          11.378          4.7123          5.2735
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              903:        0.88862E-01

===============================================================


 INSTANT    0.904000000E+03   TIME STEP NUMBER             904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000437E+04
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 :  0.23773E+00 0.13264E+01
   Friction velocity        uet   :  0.14217E-01 0.79043E-01
   Friction velocity        uk    :  0.17457E-01 0.38614E-01
   Dimensionless distance   yplus :  0.42914E+03 0.94554E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57174E+01      55   0.13634E-02   0.18745E-01 
c  VelocityX    0.46299E+04      13   0.67463E-02   0.36440E-03 
c  VelocityY    0.46299E+04      13   0.67463E-02   0.22182E-04 
c  VelocityZ    0.46299E+04      13   0.67463E-02   0.40404E-04 
c  TurbEner     0.59776E+01      13   0.10343E-03   0.98619E-09 
c  Dissip       0.15694E+01      16   0.19676E-02   0.43153E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.93           54530           26776           27271
v  Velocity[x]            0.29265          2.0212         0.90805         0.90982
v  Velocity[y]           -0.38218         0.70112      0.00055457       0.0003316
v  Velocity[z]           -0.42165         0.51109      -0.0012509      -0.0013768
v  TurbEner             0.0010176        0.015542       0.0032862       0.0033456
v  Dissip               9.209e-05        0.033924      0.00045298      0.00039142
v  TurbVisc               0.16566          11.359          4.7122          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              904:        0.89779E-01

===============================================================


 INSTANT    0.905000000E+03   TIME STEP NUMBER             905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999275E+04
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 :  0.23809E+00 0.12211E+01
   Friction velocity        uet   :  0.14238E-01 0.72347E-01
   Friction velocity        uk    :  0.17472E-01 0.38598E-01
   Dimensionless distance   yplus :  0.42863E+03 0.94499E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67524E+01      57   0.14357E-02   0.22128E-01 
c  VelocityX    0.46298E+04      12   0.68152E-02   0.34851E-03 
c  VelocityY    0.46298E+04      12   0.68152E-02   0.47387E-04 
c  VelocityZ    0.46298E+04      12   0.68152E-02   0.10844E-03 
c  TurbEner     0.59765E+01      13   0.15365E-03   0.21406E-08 
c  Dissip       0.15320E+01      17   0.24971E-02   0.88409E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.82           54542           26776           27270
v  Velocity[x]            0.29279          2.1012         0.90803         0.90981
v  Velocity[y]            -0.3669         0.70931      0.00056907      0.00034163
v  Velocity[z]           -0.42069         0.50481      -0.0012333      -0.0013569
v  TurbEner             0.0010199        0.014879       0.0032861       0.0033455
v  Dissip              9.2153e-05        0.032296      0.00045272      0.00039124
v  TurbVisc               0.16541           11.36          4.7122          5.2734
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              905:        0.89918E-01

===============================================================


 INSTANT    0.906000000E+03   TIME STEP NUMBER             906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001122E+04
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 :  0.23786E+00 0.13255E+01
   Friction velocity        uet   :  0.14225E-01 0.78995E-01
   Friction velocity        uk    :  0.17492E-01 0.38449E-01
   Dimensionless distance   yplus :  0.42965E+03 0.94472E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68026E+01      56   0.13740E-02   0.22315E-01 
c  VelocityX    0.46298E+04      12   0.67791E-02   0.29556E-03 
c  VelocityY    0.46298E+04      12   0.67791E-02   0.68626E-04 
c  VelocityZ    0.46298E+04      12   0.67791E-02   0.56717E-04 
c  TurbEner     0.59763E+01      13   0.70580E-04   0.98520E-09 
c  Dissip       0.15261E+01      14   0.67505E-03   0.61560E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.44           54548           26776           27270
v  Velocity[x]            0.29289          2.1413         0.90805         0.90983
v  Velocity[y]            -0.3824         0.69995      0.00055579      0.00033192
v  Velocity[z]           -0.42109         0.51174      -0.0012484      -0.0013723
v  TurbEner             0.0010157        0.014783       0.0032859       0.0033454
v  Dissip              9.2181e-05        0.031851      0.00045265      0.00039119
v  TurbVisc               0.16596          11.335          4.7123          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              906:        0.89545E-01

===============================================================


 INSTANT    0.907000000E+03   TIME STEP NUMBER             907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000522E+04
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 :  0.23797E+00 0.12168E+01
   Friction velocity        uet   :  0.14232E-01 0.72517E-01
   Friction velocity        uk    :  0.17456E-01 0.38462E-01
   Dimensionless distance   yplus :  0.42914E+03 0.94473E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68522E+01      68   0.14774E-02   0.22463E-01 
c  VelocityX    0.46300E+04      12   0.76412E-02   0.34432E-03 
c  VelocityY    0.46300E+04      12   0.76412E-02   0.42079E-04 
c  VelocityZ    0.46300E+04      12   0.76412E-02   0.27772E-04 
c  TurbEner     0.59774E+01      13   0.65180E-04   0.72944E-09 
c  Dissip       0.15417E+01      14   0.58869E-03   0.85149E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.09           54541           26776           27270
v  Velocity[x]            0.29258          2.1861         0.90806         0.90984
v  Velocity[y]           -0.36693         0.70617      0.00056091      0.00033736
v  Velocity[z]           -0.42117         0.50566      -0.0012398       -0.001362
v  TurbEner              0.001018        0.014872        0.003286       0.0033454
v  Dissip                9.22e-05        0.031975      0.00045278      0.00039127
v  TurbVisc               0.16556          11.331          4.7122          5.2734
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              907:        0.91550E-01

===============================================================


 INSTANT    0.908000000E+03   TIME STEP NUMBER             908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000978E+04
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 :  0.23769E+00 0.13248E+01
   Friction velocity        uet   :  0.14215E-01 0.78948E-01
   Friction velocity        uk    :  0.17476E-01 0.38551E-01
   Dimensionless distance   yplus :  0.42883E+03 0.94494E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70459E+01      59   0.16795E-02   0.23096E-01 
c  VelocityX    0.46298E+04      12   0.72441E-02   0.50830E-03 
c  VelocityY    0.46298E+04      12   0.72441E-02   0.35984E-04 
c  VelocityZ    0.46298E+04      12   0.72441E-02   0.40546E-04 
c  TurbEner     0.59779E+01      13   0.12628E-03   0.17373E-08 
c  Dissip       0.15504E+01      16   0.18263E-02   0.35207E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.56           54517           26776           27270
v  Velocity[x]            0.29276          2.0119         0.90806         0.90984
v  Velocity[y]           -0.38282         0.70132      0.00055718       0.0003391
v  Velocity[z]           -0.42031         0.51047      -0.0012332      -0.0013559
v  TurbEner             0.0010181        0.015444       0.0032861       0.0033456
v  Dissip              9.2168e-05          0.0334      0.00045291      0.00039139
v  TurbVisc               0.16542          11.357          4.7122          5.2734
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              908:        0.90720E-01

===============================================================


 INSTANT    0.909000000E+03   TIME STEP NUMBER             909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999898E+04
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 :  0.23713E+00 0.12524E+01
   Friction velocity        uet   :  0.14182E-01 0.73048E-01
   Friction velocity        uk    :  0.17477E-01 0.38583E-01
   Dimensionless distance   yplus :  0.42933E+03 0.94521E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61431E+01      54   0.13370E-02   0.20151E-01 
c  VelocityX    0.46299E+04      13   0.68517E-02   0.40291E-03 
c  VelocityY    0.46299E+04      13   0.68517E-02   0.27115E-04 
c  VelocityZ    0.46299E+04      13   0.68517E-02   0.52473E-04 
c  TurbEner     0.59762E+01      13   0.13386E-03   0.20791E-08 
c  Dissip       0.15096E+01      16   0.23396E-02   0.79465E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.05           54525           26775           27270
v  Velocity[x]            0.29271          2.0915         0.90805         0.90982
v  Velocity[y]           -0.36737         0.70882       0.0005561      0.00033271
v  Velocity[z]           -0.41987         0.50427      -0.0012446      -0.0013657
v  TurbEner             0.0010148        0.014873       0.0032858       0.0033454
v  Dissip              9.2148e-05        0.031915      0.00045262      0.00039119
v  TurbVisc                0.1657          11.339          4.7122          5.2735
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              909:        0.89744E-01

===============================================================


 INSTANT    0.910000000E+03   TIME STEP NUMBER             910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000586E+04
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 :  0.23802E+00 0.13250E+01
   Friction velocity        uet   :  0.14236E-01 0.78973E-01
   Friction velocity        uk    :  0.17448E-01 0.38585E-01
   Dimensionless distance   yplus :  0.42905E+03 0.94566E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61181E+01      56   0.13420E-02   0.20051E-01 
c  VelocityX    0.46298E+04      12   0.69624E-02   0.38223E-03 
c  VelocityY    0.46298E+04      12   0.69624E-02   0.29191E-04 
c  VelocityZ    0.46298E+04      12   0.69624E-02   0.53281E-04 
c  TurbEner     0.59765E+01      13   0.66963E-04   0.80619E-09 
c  Dissip       0.15098E+01      14   0.68691E-03   0.52478E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.6           54524           26775           27270
v  Velocity[x]            0.29285           2.143         0.90806         0.90983
v  Velocity[y]           -0.38225         0.69814      0.00055665      0.00033411
v  Velocity[z]            -0.4215         0.51188      -0.0012484       -0.001371
v  TurbEner              0.001015        0.014751       0.0032858       0.0033454
v  Dissip              9.2064e-05        0.031434      0.00045253      0.00039112
v  TurbVisc               0.16544          11.352          4.7122          5.2734
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              910:        0.89426E-01

===============================================================


 INSTANT    0.911000000E+03   TIME STEP NUMBER             911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999994E+04
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 :  0.23785E+00 0.12175E+01
   Friction velocity        uet   :  0.14226E-01 0.72560E-01
   Friction velocity        uk    :  0.17450E-01 0.38538E-01
   Dimensionless distance   yplus :  0.42820E+03 0.94570E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67458E+01      56   0.15177E-02   0.22123E-01 
c  VelocityX    0.46299E+04      12   0.71662E-02   0.34010E-03 
c  VelocityY    0.46299E+04      12   0.71662E-02   0.66626E-04 
c  VelocityZ    0.46299E+04      12   0.71662E-02   0.11619E-03 
c  TurbEner     0.59774E+01      12   0.72556E-04   0.85151E-09 
c  Dissip       0.15272E+01      15   0.65598E-03   0.10665E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.38           54529           26775           27270
v  Velocity[x]              0.293          2.1902         0.90805         0.90983
v  Velocity[y]           -0.36603         0.70618      0.00057209      0.00034821
v  Velocity[z]           -0.41976         0.50652      -0.0012232      -0.0013454
v  TurbEner             0.0010157        0.014848       0.0032859       0.0033454
v  Dissip              9.2054e-05        0.031496      0.00045262      0.00039118
v  TurbVisc               0.16502          11.333          4.7122          5.2735
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              911:        0.89134E-01

===============================================================


 INSTANT    0.912000000E+03   TIME STEP NUMBER             912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000534E+04
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 :  0.23779E+00 0.13247E+01
   Friction velocity        uet   :  0.14223E-01 0.78949E-01
   Friction velocity        uk    :  0.17456E-01 0.38601E-01
   Dimensionless distance   yplus :  0.42883E+03 0.94511E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62790E+01      63   0.14179E-02   0.20595E-01 
c  VelocityX    0.46298E+04      12   0.68277E-02   0.38842E-03 
c  VelocityY    0.46298E+04      12   0.68277E-02   0.25079E-04 
c  VelocityZ    0.46298E+04      12   0.68277E-02   0.54050E-04 
c  TurbEner     0.59771E+01      13   0.13639E-03   0.18885E-08 
c  Dissip       0.15370E+01      16   0.19719E-02   0.43552E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.52           54515           26776           27270
v  Velocity[x]            0.29258          2.0197         0.90806         0.90983
v  Velocity[y]           -0.38222         0.70238       0.0005609      0.00033933
v  Velocity[z]            -0.4214         0.51105      -0.0012423      -0.0013675
v  TurbEner             0.0010109        0.015485       0.0032858       0.0033453
v  Dissip              9.2004e-05        0.033024      0.00045272      0.00039124
v  TurbVisc               0.16536          11.329          4.7122          5.2735
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              912:        0.90355E-01

===============================================================


 INSTANT    0.913000000E+03   TIME STEP NUMBER             913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999243E+04
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 :  0.23782E+00 0.12540E+01
   Friction velocity        uet   :  0.14226E-01 0.72966E-01
   Friction velocity        uk    :  0.17415E-01 0.38558E-01
   Dimensionless distance   yplus :  0.42815E+03 0.94465E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65443E+01      58   0.14142E-02   0.21448E-01 
c  VelocityX    0.46299E+04      13   0.72063E-02   0.37182E-03 
c  VelocityY    0.46299E+04      13   0.72063E-02   0.24213E-04 
c  VelocityZ    0.46299E+04      13   0.72063E-02   0.49838E-04 
c  TurbEner     0.59756E+01      14   0.12993E-03   0.18766E-08 
c  Dissip       0.14997E+01      16   0.21668E-02   0.71851E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.53           54518           26775           27269
v  Velocity[x]            0.29269          2.0969         0.90807         0.90984
v  Velocity[y]           -0.36763         0.71074      0.00055841       0.0003333
v  Velocity[z]           -0.42312         0.50426      -0.0012326      -0.0013552
v  TurbEner             0.0010129        0.014937       0.0032854        0.003345
v  Dissip               9.201e-05        0.031678      0.00045237      0.00039099
v  TurbVisc               0.16488          11.361          4.7122          5.2735
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              913:        0.89427E-01

===============================================================


 INSTANT    0.914000000E+03   TIME STEP NUMBER             914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000385E+04
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 :  0.23773E+00 0.13252E+01
   Friction velocity        uet   :  0.14220E-01 0.78980E-01
   Friction velocity        uk    :  0.17432E-01 0.38577E-01
   Dimensionless distance   yplus :  0.42782E+03 0.94403E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66196E+01      60   0.15403E-02   0.21699E-01 
c  VelocityX    0.46298E+04      12   0.65607E-02   0.42971E-03 
c  VelocityY    0.46298E+04      12   0.65607E-02   0.30067E-04 
c  VelocityZ    0.46298E+04      12   0.65607E-02   0.51809E-04 
c  TurbEner     0.59758E+01      12   0.70051E-04   0.83451E-09 
c  Dissip       0.15058E+01      14   0.49120E-03   0.36097E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.09           54504           26776           27270
v  Velocity[x]            0.29297          2.1466         0.90806         0.90984
v  Velocity[y]           -0.38239         0.69761      0.00056713      0.00034572
v  Velocity[z]           -0.41915         0.51169      -0.0012351      -0.0013578
v  TurbEner             0.0010124        0.014824       0.0032852       0.0033449
v  Dissip              9.1996e-05        0.031385      0.00045226       0.0003909
v  TurbVisc               0.16472          11.341           4.712          5.2733
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              914:        0.89511E-01

===============================================================


 INSTANT    0.915000000E+03   TIME STEP NUMBER             915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998399E+04
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 :  0.23750E+00 0.12193E+01
   Friction velocity        uet   :  0.14206E-01 0.72659E-01
   Friction velocity        uk    :  0.17428E-01 0.38586E-01
   Dimensionless distance   yplus :  0.42821E+03 0.94403E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72015E+01      58   0.13656E-02   0.23615E-01 
c  VelocityX    0.46299E+04      12   0.65254E-02   0.32083E-03 
c  VelocityY    0.46299E+04      12   0.65254E-02   0.46214E-04 
c  VelocityZ    0.46299E+04      12   0.65254E-02   0.95516E-04 
c  TurbEner     0.59759E+01      13   0.71852E-04   0.10100E-08 
c  Dissip       0.15265E+01      15   0.71978E-03   0.13214E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.12           54534           26776           27270
v  Velocity[x]            0.29261          2.1928         0.90805         0.90982
v  Velocity[y]           -0.36659         0.70664      0.00056955      0.00034358
v  Velocity[z]           -0.42088         0.50593      -0.0012229      -0.0013444
v  TurbEner             0.0010089        0.014871        0.003285       0.0033447
v  Dissip               9.201e-05        0.031494      0.00045231      0.00039092
v  TurbVisc               0.16489           11.34          4.7121          5.2734
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              915:        0.89758E-01

===============================================================


 INSTANT    0.916000000E+03   TIME STEP NUMBER             916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999579E+04
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 :  0.23779E+00 0.13240E+01
   Friction velocity        uet   :  0.14224E-01 0.78896E-01
   Friction velocity        uk    :  0.17397E-01 0.38524E-01
   Dimensionless distance   yplus :  0.42789E+03 0.94319E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68200E+01      58   0.14313E-02   0.22375E-01 
c  VelocityX    0.46297E+04      12   0.66926E-02   0.37070E-03 
c  VelocityY    0.46297E+04      12   0.66926E-02   0.31263E-04 
c  VelocityZ    0.46297E+04      12   0.66926E-02   0.51285E-04 
c  TurbEner     0.59760E+01      13   0.13019E-03   0.13751E-08 
c  Dissip       0.15314E+01      16   0.19025E-02   0.38564E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.51           54526           26777           27271
v  Velocity[x]            0.29264          2.0106         0.90803         0.90981
v  Velocity[y]           -0.38228          0.7008      0.00056627      0.00034191
v  Velocity[z]           -0.42047         0.51104      -0.0012385      -0.0013632
v  TurbEner             0.0010089        0.015499        0.003285       0.0033446
v  Dissip              9.2012e-05        0.032982      0.00045237      0.00039095
v  TurbVisc               0.16444          11.302           4.712          5.2733
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              916:        0.90056E-01

===============================================================


 INSTANT    0.917000000E+03   TIME STEP NUMBER             917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998752E+04
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 :  0.23819E+00 0.12176E+01
   Friction velocity        uet   :  0.14249E-01 0.72567E-01
   Friction velocity        uk    :  0.17397E-01 0.38563E-01
   Dimensionless distance   yplus :  0.42706E+03 0.94299E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56740E+01      53   0.11744E-02   0.18596E-01 
c  VelocityX    0.46298E+04      12   0.66705E-02   0.35232E-03 
c  VelocityY    0.46298E+04      12   0.66705E-02   0.22055E-04 
c  VelocityZ    0.46298E+04      12   0.66705E-02   0.35357E-04 
c  TurbEner     0.59744E+01      13   0.15878E-03   0.21641E-08 
c  Dissip       0.14874E+01      17   0.26541E-02   0.91162E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.86           54538           26776           27270
v  Velocity[x]            0.29267          2.1035         0.90805         0.90982
v  Velocity[y]           -0.36696         0.70863      0.00056007        0.000333
v  Velocity[z]           -0.42141         0.50471      -0.0012388      -0.0013619
v  TurbEner             0.0010098        0.014746       0.0032846       0.0033443
v  Dissip              9.2033e-05        0.031171      0.00045197      0.00039067
v  TurbVisc               0.16411          11.303           4.712          5.2734
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              917:        0.89663E-01

===============================================================


 INSTANT    0.918000000E+03   TIME STEP NUMBER             918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001085E+04
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 :  0.23766E+00 0.13240E+01
   Friction velocity        uet   :  0.14217E-01 0.78903E-01
   Friction velocity        uk    :  0.17406E-01 0.38594E-01
   Dimensionless distance   yplus :  0.42783E+03 0.94362E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57580E+01      56   0.12871E-02   0.18891E-01 
c  VelocityX    0.46299E+04      12   0.72300E-02   0.30583E-03 
c  VelocityY    0.46299E+04      12   0.72300E-02   0.21606E-04 
c  VelocityZ    0.46299E+04      12   0.72300E-02   0.38406E-04 
c  TurbEner     0.59746E+01      12   0.60002E-04   0.51240E-09 
c  Dissip       0.14889E+01      13   0.42819E-03   0.27241E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.47           54548           26776           27271
v  Velocity[x]            0.29272          2.1479         0.90805         0.90983
v  Velocity[y]           -0.38244          0.7002      0.00055203      0.00032813
v  Velocity[z]           -0.42202         0.51175      -0.0012428      -0.0013646
v  TurbEner             0.0010035        0.014663       0.0032845       0.0033442
v  Dissip              9.2017e-05        0.030904      0.00045182      0.00039056
v  TurbVisc               0.16449          11.338           4.712          5.2733
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              918:        0.90299E-01

===============================================================


 INSTANT    0.919000000E+03   TIME STEP NUMBER             919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999755E+04
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 :  0.23775E+00 0.12171E+01
   Friction velocity        uet   :  0.14223E-01 0.72536E-01
   Friction velocity        uk    :  0.17351E-01 0.38495E-01
   Dimensionless distance   yplus :  0.42730E+03 0.94328E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63052E+01      65   0.12361E-02   0.20651E-01 
c  VelocityX    0.46298E+04      12   0.73298E-02   0.36260E-03 
c  VelocityY    0.46298E+04      12   0.73298E-02   0.24025E-04 
c  VelocityZ    0.46298E+04      12   0.73298E-02   0.10119E-03 
c  TurbEner     0.59754E+01      13   0.66647E-04   0.78697E-09 
c  Dissip       0.15083E+01      14   0.65142E-03   0.93989E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.79           54550           26775           27269
v  Velocity[x]             0.2928          2.1815         0.90804         0.90981
v  Velocity[y]           -0.36689         0.70675      0.00056789      0.00034158
v  Velocity[z]           -0.42159          0.5057      -0.0012385      -0.0013635
v  TurbEner             0.0010026         0.01482       0.0032845       0.0033442
v  Dissip              9.1997e-05        0.031188      0.00045187      0.00039059
v  TurbVisc               0.16363          11.327           4.712          5.2733
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              919:        0.93755E-01

===============================================================


 INSTANT    0.920000000E+03   TIME STEP NUMBER             920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002201E+04
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 :  0.23775E+00 0.13254E+01
   Friction velocity        uet   :  0.14223E-01 0.78981E-01
   Friction velocity        uk    :  0.17343E-01 0.38503E-01
   Dimensionless distance   yplus :  0.42611E+03 0.94304E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64835E+01      59   0.14869E-02   0.21252E-01 
c  VelocityX    0.46298E+04      12   0.74234E-02   0.35979E-03 
c  VelocityY    0.46298E+04      12   0.74234E-02   0.39793E-04 
c  VelocityZ    0.46298E+04      12   0.74234E-02   0.52788E-04 
c  TurbEner     0.59767E+01      13   0.83060E-04   0.11043E-08 
c  Dissip       0.15290E+01      15   0.85630E-03   0.16154E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.71           54543           26776           27270
v  Velocity[x]            0.29275          2.1982         0.90806         0.90984
v  Velocity[y]           -0.38281         0.69997      0.00055855      0.00033769
v  Velocity[z]           -0.41927         0.51045      -0.0012336      -0.0013569
v  TurbEner             0.0010017        0.015003       0.0032847       0.0033444
v  Dissip              9.1986e-05        0.031595      0.00045205      0.00039072
v  TurbVisc               0.16339          11.324           4.712          5.2733
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              920:        0.91744E-01

===============================================================


 INSTANT    0.921000000E+03   TIME STEP NUMBER             921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000340E+04
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 :  0.23739E+00 0.12141E+01
   Friction velocity        uet   :  0.14202E-01 0.72354E-01
   Friction velocity        uk    :  0.17335E-01 0.38535E-01
   Dimensionless distance   yplus :  0.42622E+03 0.94276E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.78261E+01      60   0.19166E-02   0.25658E-01 
c  VelocityX    0.46298E+04      13   0.69981E-02   0.46322E-03 
c  VelocityY    0.46298E+04      13   0.69981E-02   0.48392E-04 
c  VelocityZ    0.46298E+04      13   0.69981E-02   0.29681E-04 
c  TurbEner     0.59777E+01      13   0.12931E-03   0.16908E-08 
c  Dissip       0.15498E+01      16   0.22340E-02   0.55503E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.13           54516           26775           27270
v  Velocity[x]            0.29257          2.0431         0.90805         0.90982
v  Velocity[y]           -0.36735         0.70808      0.00056711      0.00034579
v  Velocity[z]           -0.41999         0.50437      -0.0012302      -0.0013533
v  TurbEner            0.00099767        0.015608       0.0032849       0.0033445
v  Dissip              9.2012e-05         0.03337       0.0004523      0.00039091
v  TurbVisc               0.16352          11.357          4.7121          5.2734
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              921:        0.90801E-01

===============================================================


 INSTANT    0.922000000E+03   TIME STEP NUMBER             922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000644E+04
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 :  0.23775E+00 0.13252E+01
   Friction velocity        uet   :  0.14225E-01 0.78982E-01
   Friction velocity        uk    :  0.17300E-01 0.38560E-01
   Dimensionless distance   yplus :  0.42619E+03 0.94241E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63557E+01      55   0.13742E-02   0.20841E-01 
c  VelocityX    0.46298E+04      12   0.67426E-02   0.35639E-03 
c  VelocityY    0.46298E+04      12   0.67426E-02   0.31982E-04 
c  VelocityZ    0.46298E+04      12   0.67426E-02   0.41288E-04 
c  TurbEner     0.59758E+01      13   0.13210E-03   0.18515E-08 
c  Dissip       0.15222E+01      16   0.19060E-02   0.51695E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.15           54524           26776           27270
v  Velocity[x]            0.29281           2.104         0.90805         0.90983
v  Velocity[y]           -0.38218         0.69917      0.00055275      0.00033266
v  Velocity[z]           -0.42087         0.51192      -0.0012331      -0.0013575
v  TurbEner            0.00099704        0.015036       0.0032848       0.0033445
v  Dissip              9.2045e-05        0.032078      0.00045215      0.00039081
v  TurbVisc               0.16309          11.332          4.7121          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              922:        0.92698E-01

===============================================================


 INSTANT    0.923000000E+03   TIME STEP NUMBER             923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998690E+04
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 :  0.23797E+00 0.12235E+01
   Friction velocity        uet   :  0.14238E-01 0.72473E-01
   Friction velocity        uk    :  0.17295E-01 0.38575E-01
   Dimensionless distance   yplus :  0.42491E+03 0.94153E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60444E+01      55   0.13073E-02   0.19807E-01 
c  VelocityX    0.46299E+04      12   0.77096E-02   0.34457E-03 
c  VelocityY    0.46299E+04      12   0.77096E-02   0.26527E-04 
c  VelocityZ    0.46299E+04      12   0.77096E-02   0.56070E-04 
c  TurbEner     0.59762E+01      13   0.61998E-04   0.68678E-09 
c  Dissip       0.15274E+01      13   0.22635E-03   0.13168E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.52           54523           26775           27269
v  Velocity[x]            0.29301          2.1554         0.90806         0.90983
v  Velocity[y]           -0.36611         0.70583      0.00056583       0.0003418
v  Velocity[z]           -0.42201         0.50644      -0.0012313      -0.0013544
v  TurbEner            0.00099858        0.014985       0.0032847       0.0033444
v  Dissip              9.2041e-05        0.031993      0.00045217      0.00039082
v  TurbVisc               0.16286          11.331          4.7121          5.2734
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              923:        0.90297E-01

===============================================================


 INSTANT    0.924000000E+03   TIME STEP NUMBER             924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000573E+04
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 :  0.23748E+00 0.13250E+01
   Friction velocity        uet   :  0.14210E-01 0.78969E-01
   Friction velocity        uk    :  0.17308E-01 0.38555E-01
   Dimensionless distance   yplus :  0.42553E+03 0.94180E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62861E+01      57   0.15692E-02   0.20626E-01 
c  VelocityX    0.46299E+04      12   0.71367E-02   0.37505E-03 
c  VelocityY    0.46299E+04      12   0.71367E-02   0.28733E-04 
c  VelocityZ    0.46299E+04      12   0.71367E-02   0.56355E-04 
c  TurbEner     0.59768E+01      13   0.76479E-04   0.10839E-08 
c  Dissip       0.15484E+01      15   0.78725E-03   0.15880E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.17           54513           26776           27270
v  Velocity[x]            0.29271          2.1864         0.90807         0.90985
v  Velocity[y]           -0.38226         0.70117      0.00056058       0.0003413
v  Velocity[z]           -0.42066          0.5111       -0.001239      -0.0013617
v  TurbEner             0.0009948        0.015064       0.0032849       0.0033445
v  Dissip              9.2072e-05        0.032168      0.00045238      0.00039096
v  TurbVisc               0.16334          11.372          4.7121          5.2734
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              924:        0.90387E-01

===============================================================


 INSTANT    0.925000000E+03   TIME STEP NUMBER             925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999091E+04
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 :  0.23793E+00 0.12134E+01
   Friction velocity        uet   :  0.14237E-01 0.72324E-01
   Friction velocity        uk    :  0.17275E-01 0.38453E-01
   Dimensionless distance   yplus :  0.42543E+03 0.94174E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65606E+01      60   0.12812E-02   0.21493E-01 
c  VelocityX    0.46299E+04      12   0.73830E-02   0.38531E-03 
c  VelocityY    0.46299E+04      12   0.73830E-02   0.32088E-04 
c  VelocityZ    0.46299E+04      12   0.73830E-02   0.10632E-03 
c  TurbEner     0.59772E+01      13   0.76649E-04   0.12604E-08 
c  Dissip       0.15752E+01      15   0.84319E-03   0.14634E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.35           54528           26775           27269
v  Velocity[x]            0.29278          2.2161         0.90805         0.90982
v  Velocity[y]            -0.3677         0.70873      0.00057285      0.00034901
v  Velocity[z]           -0.42188         0.50417      -0.0012344      -0.0013591
v  TurbEner            0.00099646         0.01524       0.0032849       0.0033445
v  Dissip              9.2056e-05        0.032664      0.00045259      0.00039109
v  TurbVisc               0.16305          11.358          4.7121          5.2733
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              925:        0.90633E-01

===============================================================


 INSTANT    0.926000000E+03   TIME STEP NUMBER             926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001768E+04
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 :  0.23767E+00 0.13249E+01
   Friction velocity        uet   :  0.14222E-01 0.78970E-01
   Friction velocity        uk    :  0.17290E-01 0.38420E-01
   Dimensionless distance   yplus :  0.42468E+03 0.94215E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62791E+01      55   0.15509E-02   0.20574E-01 
c  VelocityX    0.46298E+04      12   0.73756E-02   0.46054E-03 
c  VelocityY    0.46298E+04      12   0.73756E-02   0.27333E-04 
c  VelocityZ    0.46298E+04      12   0.73756E-02   0.41979E-04 
c  TurbEner     0.59779E+01      13   0.14161E-03   0.16153E-08 
c  Dissip       0.15966E+01      16   0.24332E-02   0.67797E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.6           54515           26775           27269
v  Velocity[x]            0.29274          2.0394         0.90806         0.90983
v  Velocity[y]           -0.38244         0.69812      0.00056775      0.00034562
v  Velocity[z]           -0.41849         0.51174      -0.0012355      -0.0013591
v  TurbEner            0.00099795        0.015917        0.003285       0.0033445
v  Dissip              9.2035e-05        0.034615      0.00045288       0.0003913
v  TurbVisc                 0.163          11.364           4.712          5.2733
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              926:        0.89262E-01

===============================================================


 INSTANT    0.927000000E+03   TIME STEP NUMBER             927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000302E+04
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 :  0.23761E+00 0.12392E+01
   Friction velocity        uet   :  0.14218E-01 0.72567E-01
   Friction velocity        uk    :  0.17303E-01 0.38509E-01
   Dimensionless distance   yplus :  0.42523E+03 0.94327E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66922E+01      59   0.15365E-02   0.21957E-01 
c  VelocityX    0.46298E+04      12   0.66390E-02   0.54533E-03 
c  VelocityY    0.46298E+04      12   0.66390E-02   0.23335E-04 
c  VelocityZ    0.46298E+04      12   0.66390E-02   0.62934E-04 
c  TurbEner     0.59761E+01      14   0.12361E-03   0.22754E-08 
c  Dissip       0.15477E+01      16   0.16232E-02   0.66373E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.57           54496           26775           27269
v  Velocity[x]            0.29276          1.7358         0.90805         0.90983
v  Velocity[y]           -0.36617         0.70632      0.00056109       0.0003393
v  Velocity[z]           -0.42046         0.50632      -0.0012433      -0.0013651
v  TurbEner            0.00099716        0.015765       0.0032849       0.0033445
v  Dissip              9.2005e-05         0.03456      0.00045271      0.00039121
v  TurbVisc               0.16341          11.335          4.7119          5.2732
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              927:        0.90340E-01

===============================================================


 INSTANT    0.928000000E+03   TIME STEP NUMBER             928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999961E+04
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 :  0.23756E+00 0.13245E+01
   Friction velocity        uet   :  0.14215E-01 0.78943E-01
   Friction velocity        uk    :  0.17296E-01 0.38541E-01
   Dimensionless distance   yplus :  0.42535E+03 0.94372E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54920E+01      54   0.12139E-02   0.18009E-01 
c  VelocityX    0.46297E+04      12   0.68158E-02   0.33715E-03 
c  VelocityY    0.46297E+04      12   0.68158E-02   0.21078E-04 
c  VelocityZ    0.46297E+04      12   0.68158E-02   0.45719E-04 
c  TurbEner     0.59703E+01      15   0.42772E-03   0.90491E-08 
c  Dissip       0.13851E+01      18   0.86459E-02   0.53562E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.62           54508           26776           27270
v  Velocity[x]             0.2928           1.876         0.90804         0.90981
v  Velocity[y]           -0.38236          0.7023      0.00055899      0.00033983
v  Velocity[z]           -0.42174          0.5109      -0.0012496      -0.0013719
v  TurbEner            0.00099978        0.013522       0.0032844       0.0033441
v  Dissip              9.2057e-05        0.028583      0.00045192       0.0003906
v  TurbVisc               0.16346           11.33          4.7119          5.2732
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              928:        0.90096E-01

===============================================================


 INSTANT    0.929000000E+03   TIME STEP NUMBER             929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999214E+04
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 :  0.23785E+00 0.12289E+01
   Friction velocity        uet   :  0.14231E-01 0.72381E-01
   Friction velocity        uk    :  0.17319E-01 0.38541E-01
   Dimensionless distance   yplus :  0.42499E+03 0.94422E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67675E+01      54   0.15220E-02   0.22188E-01 
c  VelocityX    0.46297E+04      13   0.70910E-02   0.35966E-03 
c  VelocityY    0.46297E+04      13   0.70910E-02   0.23003E-04 
c  VelocityZ    0.46297E+04      13   0.70910E-02   0.71585E-04 
c  TurbEner     0.59691E+01      14   0.16732E-03   0.24724E-08 
c  Dissip       0.13245E+01      18   0.41509E-02   0.15897E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.72           54515           26775           27270
v  Velocity[x]            0.29268          2.0044         0.90804         0.90982
v  Velocity[y]           -0.36794          0.7109      0.00056793        0.000343
v  Velocity[z]           -0.42094         0.50404      -0.0012349      -0.0013552
v  TurbEner             0.0010036        0.012747        0.003284       0.0033438
v  Dissip              9.2081e-05        0.025965      0.00045115      0.00039006
v  TurbVisc               0.16335          11.368          4.7118          5.2731
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              929:        0.90257E-01

===============================================================


 INSTANT    0.930000000E+03   TIME STEP NUMBER             930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999620E+04
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 :  0.23770E+00 0.13251E+01
   Friction velocity        uet   :  0.14222E-01 0.78974E-01
   Friction velocity        uk    :  0.17352E-01 0.38448E-01
   Dimensionless distance   yplus :  0.42635E+03 0.94457E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73680E+01      57   0.16884E-02   0.24179E-01 
c  VelocityX    0.46298E+04      12   0.61730E-02   0.33379E-03 
c  VelocityY    0.46298E+04      12   0.61730E-02   0.39612E-04 
c  VelocityZ    0.46298E+04      12   0.61730E-02   0.39708E-04 
c  TurbEner     0.59683E+01      13   0.10158E-03   0.18220E-08 
c  Dissip       0.12837E+01      18   0.24986E-02   0.96158E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.69           54494           26777           27271
v  Velocity[x]            0.29252          2.0655         0.90805         0.90983
v  Velocity[y]           -0.38302         0.69777      0.00056609      0.00034465
v  Velocity[z]           -0.42086         0.51124      -0.0012387      -0.0013607
v  TurbEner             0.0010007        0.012711       0.0032836       0.0033435
v  Dissip              9.2056e-05        0.024947      0.00045037      0.00038951
v  TurbVisc               0.16409           11.35          4.7118          5.2731
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              930:        0.90234E-01

===============================================================


 INSTANT    0.931000000E+03   TIME STEP NUMBER             931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997432E+04
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 :  0.23784E+00 0.12193E+01
   Friction velocity        uet   :  0.14229E-01 0.72658E-01
   Friction velocity        uk    :  0.17327E-01 0.38456E-01
   Dimensionless distance   yplus :  0.42609E+03 0.94407E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67552E+01      54   0.12970E-02   0.22141E-01 
c  VelocityX    0.46299E+04      12   0.70026E-02   0.33390E-03 
c  VelocityY    0.46299E+04      12   0.70026E-02   0.45361E-04 
c  VelocityZ    0.46299E+04      12   0.70026E-02   0.26725E-04 
c  TurbEner     0.59681E+01      13   0.64175E-04   0.84661E-09 
c  Dissip       0.12701E+01      17   0.11306E-02   0.25742E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.56           54508           26776           27270
v  Velocity[x]            0.29284          2.1322         0.90804         0.90981
v  Velocity[y]           -0.36812         0.70739      0.00056506      0.00034099
v  Velocity[z]           -0.42263          0.5069      -0.0012394      -0.0013593
v  TurbEner             0.0010043        0.012886       0.0032832       0.0033432
v  Dissip              9.2064e-05        0.024616      0.00044973      0.00038906
v  TurbVisc               0.16379          11.355          4.7118          5.2732
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              931:        0.89729E-01

===============================================================


 INSTANT    0.932000000E+03   TIME STEP NUMBER             932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000763E+04
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 :  0.23756E+00 0.13243E+01
   Friction velocity        uet   :  0.14212E-01 0.78918E-01
   Friction velocity        uk    :  0.17358E-01 0.38538E-01
   Dimensionless distance   yplus :  0.42606E+03 0.94397E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66427E+01      52   0.13675E-02   0.21768E-01 
c  VelocityX    0.46298E+04      12   0.72718E-02   0.39232E-03 
c  VelocityY    0.46298E+04      12   0.72718E-02   0.36159E-04 
c  VelocityZ    0.46298E+04      12   0.72718E-02   0.43507E-04 
c  TurbEner     0.59695E+01      13   0.99884E-04   0.13120E-08 
c  Dissip       0.12757E+01      16   0.62253E-03   0.77137E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.15           54514           26776           27270
v  Velocity[x]            0.29293          2.1615         0.90806         0.90983
v  Velocity[y]           -0.38284         0.70173      0.00055917      0.00033799
v  Velocity[z]           -0.41877         0.51378      -0.0012394      -0.0013623
v  TurbEner             0.0010059        0.013319       0.0032833       0.0033433
v  Dissip              9.2072e-05         0.02494      0.00044934      0.00038878
v  TurbVisc               0.16385          11.328          4.7119          5.2732
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              932:        0.89010E-01

===============================================================


 INSTANT    0.933000000E+03   TIME STEP NUMBER             933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001005E+04
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 :  0.23749E+00 0.12427E+01
   Friction velocity        uet   :  0.14208E-01 0.72615E-01
   Friction velocity        uk    :  0.17372E-01 0.38573E-01
   Dimensionless distance   yplus :  0.42681E+03 0.94430E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65757E+01      59   0.16807E-02   0.21571E-01 
c  VelocityX    0.46299E+04      12   0.66091E-02   0.41519E-03 
c  VelocityY    0.46299E+04      12   0.66091E-02   0.32225E-04 
c  VelocityZ    0.46299E+04      12   0.66091E-02   0.33693E-04 
c  TurbEner     0.59706E+01      13   0.14235E-03   0.21137E-08 
c  Dissip       0.12895E+01      16   0.18851E-02   0.35263E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.69           54498           26776           27270
v  Velocity[x]            0.29258          2.0162         0.90807         0.90983
v  Velocity[y]           -0.36643         0.70931       0.0005638      0.00034247
v  Velocity[z]           -0.42038         0.50794      -0.0012339      -0.0013541
v  TurbEner             0.0010045        0.014077       0.0032833       0.0033433
v  Dissip              9.2067e-05        0.026325      0.00044915      0.00038866
v  TurbVisc               0.16425          11.325          4.7122          5.2735
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              933:        0.89865E-01

===============================================================


 INSTANT    0.934000000E+03   TIME STEP NUMBER             934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001221E+04
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 :  0.23765E+00 0.13242E+01
   Friction velocity        uet   :  0.14217E-01 0.78918E-01
   Friction velocity        uk    :  0.17359E-01 0.38561E-01
   Dimensionless distance   yplus :  0.42689E+03 0.94393E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63191E+01      54   0.13041E-02   0.20722E-01 
c  VelocityX    0.46298E+04      12   0.67313E-02   0.34928E-03 
c  VelocityY    0.46298E+04      12   0.67313E-02   0.28247E-04 
c  VelocityZ    0.46298E+04      12   0.67313E-02   0.40408E-04 
c  TurbEner     0.59696E+01      13   0.77133E-04   0.10875E-08 
c  Dissip       0.12670E+01      16   0.15573E-02   0.32588E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.31           54507           26776           27271
v  Velocity[x]            0.29272           2.086         0.90806         0.90982
v  Velocity[y]           -0.38262         0.70083      0.00055547       0.0003349
v  Velocity[z]           -0.42015          0.5121      -0.0012407      -0.0013625
v  TurbEner             0.0010066        0.013793       0.0032832       0.0033432
v  Dissip              9.2074e-05        0.025355       0.0004487      0.00038835
v  TurbVisc               0.16415          11.354          4.7123          5.2736
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              934:        0.89523E-01

===============================================================


 INSTANT    0.935000000E+03   TIME STEP NUMBER             935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998193E+04
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 :  0.23817E+00 0.12176E+01
   Friction velocity        uet   :  0.14249E-01 0.72561E-01
   Friction velocity        uk    :  0.17377E-01 0.38449E-01
   Dimensionless distance   yplus :  0.42641E+03 0.94365E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61599E+01      54   0.14164E-02   0.20186E-01 
c  VelocityX    0.46299E+04      12   0.74373E-02   0.32709E-03 
c  VelocityY    0.46299E+04      12   0.74373E-02   0.32196E-04 
c  VelocityZ    0.46299E+04      12   0.74373E-02   0.12324E-03 
c  TurbEner     0.59707E+01      13   0.74928E-04   0.92125E-09 
c  Dissip       0.12786E+01      14   0.34668E-03   0.28730E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.35           54523           26776           27270
v  Velocity[x]            0.29296          2.1378         0.90804         0.90982
v  Velocity[y]           -0.36815         0.70699       0.0005705       0.0003428
v  Velocity[z]           -0.42089         0.50491      -0.0012275      -0.0013473
v  TurbEner              0.001009        0.014028       0.0032832       0.0033432
v  Dissip              9.2091e-05         0.02552      0.00044858      0.00038827
v  TurbVisc               0.16393          11.337          4.7125          5.2738
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              935:        0.89514E-01

===============================================================


 INSTANT    0.936000000E+03   TIME STEP NUMBER             936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000267E+04
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 :  0.23758E+00 0.13261E+01
   Friction velocity        uet   :  0.14214E-01 0.79022E-01
   Friction velocity        uk    :  0.17398E-01 0.38520E-01
   Dimensionless distance   yplus :  0.42742E+03 0.94341E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69823E+01      57   0.15873E-02   0.22901E-01 
c  VelocityX    0.46300E+04      12   0.72955E-02   0.42836E-03 
c  VelocityY    0.46300E+04      12   0.72955E-02   0.28028E-04 
c  VelocityZ    0.46300E+04      12   0.72955E-02   0.55143E-04 
c  TurbEner     0.59724E+01      13   0.10745E-03   0.18467E-08 
c  Dissip       0.13009E+01      16   0.11597E-02   0.29420E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.15           54514           26777           27271
v  Velocity[x]            0.29277          2.1692         0.90807         0.90985
v  Velocity[y]            -0.3825          0.6997      0.00056182      0.00033796
v  Velocity[z]           -0.42172         0.51227      -0.0012401       -0.001362
v  TurbEner             0.0010054        0.014317       0.0032835       0.0033435
v  Dissip              9.2122e-05        0.025962      0.00044867      0.00038834
v  TurbVisc               0.16446          11.344          4.7127           5.274
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              936:        0.89951E-01

===============================================================


 INSTANT    0.937000000E+03   TIME STEP NUMBER             937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998571E+04
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 :  0.23764E+00 0.12291E+01
   Friction velocity        uet   :  0.14218E-01 0.72332E-01
   Friction velocity        uk    :  0.17368E-01 0.38495E-01
   Dimensionless distance   yplus :  0.42698E+03 0.94343E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72080E+01      66   0.14974E-02   0.23631E-01 
c  VelocityX    0.46300E+04      12   0.69394E-02   0.41218E-03 
c  VelocityY    0.46300E+04      12   0.69394E-02   0.45396E-04 
c  VelocityZ    0.46300E+04      12   0.69394E-02   0.58849E-04 
c  TurbEner     0.59731E+01      14   0.14478E-03   0.23921E-08 
c  Dissip       0.13237E+01      16   0.21575E-02   0.53389E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.79           54513           26776           27270
v  Velocity[x]            0.29274           2.013         0.90805         0.90982
v  Velocity[y]           -0.36614         0.70793      0.00057249      0.00034445
v  Velocity[z]           -0.42162         0.50688       -0.001246      -0.0013662
v  TurbEner             0.0010079        0.015078       0.0032837       0.0033436
v  Dissip              9.2117e-05         0.02762      0.00044888      0.00038849
v  TurbVisc               0.16411          11.381           4.713          5.2743
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              937:        0.90836E-01

===============================================================


 INSTANT    0.938000000E+03   TIME STEP NUMBER             938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001526E+04
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 :  0.23790E+00 0.13245E+01
   Friction velocity        uet   :  0.14234E-01 0.78941E-01
   Friction velocity        uk    :  0.17389E-01 0.38530E-01
   Dimensionless distance   yplus :  0.42680E+03 0.94305E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72558E+01      54   0.14943E-02   0.23783E-01 
c  VelocityX    0.46300E+04      12   0.74256E-02   0.40783E-03 
c  VelocityY    0.46300E+04      12   0.74256E-02   0.50284E-04 
c  VelocityZ    0.46300E+04      12   0.74256E-02   0.56082E-04 
c  TurbEner     0.59730E+01      13   0.99606E-04   0.14795E-08 
c  Dissip       0.13044E+01      16   0.15229E-02   0.34223E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.43           54513           26777           27271
v  Velocity[x]            0.29286          2.0832         0.90808         0.90986
v  Velocity[y]           -0.38246         0.69877      0.00055635      0.00033237
v  Velocity[z]           -0.41933         0.51121      -0.0012584      -0.0013786
v  TurbEner             0.0010084        0.014613       0.0032839       0.0033438
v  Dissip              9.2071e-05        0.026631      0.00044876      0.00038841
v  TurbVisc               0.16406          11.361          4.7133          5.2745
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              938:        0.89256E-01

===============================================================


 INSTANT    0.939000000E+03   TIME STEP NUMBER             939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998395E+04
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 :  0.23746E+00 0.12778E+01
   Friction velocity        uet   :  0.14209E-01 0.74496E-01
   Friction velocity        uk    :  0.17393E-01 0.38494E-01
   Dimensionless distance   yplus :  0.42733E+03 0.94307E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72307E+01      59   0.15602E-02   0.23721E-01 
c  VelocityX    0.46301E+04      12   0.67927E-02   0.40569E-03 
c  VelocityY    0.46301E+04      12   0.67927E-02   0.42713E-04 
c  VelocityZ    0.46301E+04      12   0.67927E-02   0.89054E-04 
c  TurbEner     0.59743E+01      14   0.81169E-04   0.15610E-08 
c  Dissip       0.13227E+01      15   0.42777E-03   0.53101E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.34           54526           26776           27270
v  Velocity[x]            0.29274          2.1502         0.90807         0.90984
v  Velocity[y]           -0.36821         0.70546       0.0005735      0.00034805
v  Velocity[z]           -0.41995         0.50408      -0.0012318      -0.0013521
v  TurbEner              0.001006        0.014611       0.0032844        0.003344
v  Dissip              9.2096e-05        0.026652      0.00044892      0.00038851
v  TurbVisc               0.16438          11.364          4.7135          5.2747
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              939:        0.90097E-01

===============================================================


 INSTANT    0.940000000E+03   TIME STEP NUMBER             940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000750E+04
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 :  0.23777E+00 0.13249E+01
   Friction velocity        uet   :  0.14228E-01 0.78969E-01
   Friction velocity        uk    :  0.17372E-01 0.38510E-01
   Dimensionless distance   yplus :  0.42716E+03 0.94281E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63434E+01      56   0.12740E-02   0.20801E-01 
c  VelocityX    0.46301E+04      12   0.73011E-02   0.37665E-03 
c  VelocityY    0.46301E+04      12   0.73011E-02   0.39316E-04 
c  VelocityZ    0.46301E+04      12   0.73011E-02   0.55314E-04 
c  TurbEner     0.59752E+01      14   0.98178E-04   0.22240E-08 
c  Dissip       0.13470E+01      16   0.11719E-02   0.30147E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.46           54518           26777           27271
v  Velocity[x]            0.29248           2.169         0.90807         0.90985
v  Velocity[y]           -0.38297         0.70053      0.00055827      0.00033807
v  Velocity[z]           -0.42089         0.51152      -0.0012422      -0.0013655
v  TurbEner             0.0010074        0.014868       0.0032849       0.0033443
v  Dissip              9.2103e-05        0.027233      0.00044925      0.00038872
v  TurbVisc               0.16427          11.321          4.7138          5.2749
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              940:        0.90125E-01

===============================================================


 INSTANT    0.941000000E+03   TIME STEP NUMBER             941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998958E+04
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 :  0.23790E+00 0.12345E+01
   Friction velocity        uet   :  0.14236E-01 0.72303E-01
   Friction velocity        uk    :  0.17384E-01 0.38541E-01
   Dimensionless distance   yplus :  0.42656E+03 0.94319E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62824E+01      57   0.15801E-02   0.20590E-01 
c  VelocityX    0.46302E+04      12   0.68748E-02   0.39062E-03 
c  VelocityY    0.46302E+04      12   0.68748E-02   0.27596E-04 
c  VelocityZ    0.46302E+04      12   0.68748E-02   0.37612E-04 
c  TurbEner     0.59762E+01      13   0.12866E-03   0.17439E-08 
c  Dissip       0.13691E+01      16   0.22259E-02   0.58552E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.68           54514           26777           27271
v  Velocity[x]            0.29305          2.0141         0.90805         0.90982
v  Velocity[y]           -0.36798         0.70826      0.00056201       0.0003412
v  Velocity[z]           -0.42205          0.5071      -0.0012471      -0.0013708
v  TurbEner             0.0010103        0.015544       0.0032853       0.0033445
v  Dissip              9.2081e-05        0.028992      0.00044963      0.00038899
v  TurbVisc               0.16411           11.31          4.7141          5.2751
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              941:        0.89485E-01

===============================================================


 INSTANT    0.942000000E+03   TIME STEP NUMBER             942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999488E+04
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 :  0.23744E+00 0.13249E+01
   Friction velocity        uet   :  0.14210E-01 0.78973E-01
   Friction velocity        uk    :  0.17409E-01 0.38569E-01
   Dimensionless distance   yplus :  0.42764E+03 0.94401E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61166E+01      59   0.14819E-02   0.20074E-01 
c  VelocityX    0.46302E+04      12   0.68040E-02   0.34719E-03 
c  VelocityY    0.46302E+04      12   0.68040E-02   0.25349E-04 
c  VelocityZ    0.46302E+04      12   0.68040E-02   0.47036E-04 
c  TurbEner     0.59756E+01      13   0.11885E-03   0.18218E-08 
c  Dissip       0.13542E+01      16   0.14579E-02   0.31091E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.44           54498           26778           27272
v  Velocity[x]            0.29278          2.0855         0.90808         0.90985
v  Velocity[y]           -0.38283         0.69874      0.00055952      0.00034071
v  Velocity[z]           -0.42084         0.51389      -0.0012368      -0.0013592
v  TurbEner             0.0010079        0.014968       0.0032855       0.0033448
v  Dissip              9.2043e-05         0.02799      0.00044966      0.00038901
v  TurbVisc               0.16486          11.337          4.7142          5.2752
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              942:        0.90196E-01

===============================================================


 INSTANT    0.943000000E+03   TIME STEP NUMBER             943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998038E+04
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 :  0.23793E+00 0.12267E+01
   Friction velocity        uet   :  0.14239E-01 0.72464E-01
   Friction velocity        uk    :  0.17389E-01 0.38506E-01
   Dimensionless distance   yplus :  0.42740E+03 0.94416E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61366E+01      63   0.12541E-02   0.20117E-01 
c  VelocityX    0.46302E+04      12   0.70659E-02   0.35389E-03 
c  VelocityY    0.46302E+04      12   0.70659E-02   0.49940E-04 
c  VelocityZ    0.46302E+04      12   0.70659E-02   0.10301E-03 
c  TurbEner     0.59756E+01      13   0.75513E-04   0.11694E-08 
c  Dissip       0.13683E+01      14   0.28921E-03   0.28797E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.52           54519           26777           27272
v  Velocity[x]            0.29244          2.1386         0.90805         0.90982
v  Velocity[y]           -0.36671         0.70551      0.00057347      0.00034864
v  Velocity[z]           -0.42195         0.50785       -0.001237      -0.0013611
v  TurbEner             0.0010126        0.014948       0.0032857       0.0033449
v  Dissip              9.2057e-05        0.028078      0.00044979      0.00038909
v  TurbVisc               0.16483          11.384          4.7144          5.2754
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              943:        0.90361E-01

===============================================================


 INSTANT    0.944000000E+03   TIME STEP NUMBER             944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001211E+04
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 :  0.23763E+00 0.13249E+01
   Friction velocity        uet   :  0.14222E-01 0.78963E-01
   Friction velocity        uk    :  0.17430E-01 0.38433E-01
   Dimensionless distance   yplus :  0.42753E+03 0.94408E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61778E+01      55   0.14964E-02   0.20257E-01 
c  VelocityX    0.46303E+04      12   0.72128E-02   0.37277E-03 
c  VelocityY    0.46303E+04      12   0.72128E-02   0.37167E-04 
c  VelocityZ    0.46303E+04      12   0.72128E-02   0.58339E-04 
c  TurbEner     0.59769E+01      13   0.73265E-04   0.97778E-09 
c  Dissip       0.13959E+01      16   0.11107E-02   0.28025E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.39           54515           26778           27273
v  Velocity[x]             0.2928          2.1711          0.9081         0.90987
v  Velocity[y]           -0.38269         0.69881      0.00055589      0.00033355
v  Velocity[z]           -0.41857          0.5121       -0.001241      -0.0013635
v  TurbEner             0.0010158        0.015112        0.003286       0.0033452
v  Dissip              9.2091e-05        0.028592      0.00045018      0.00038935
v  TurbVisc               0.16516          11.369          4.7145          5.2755
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              944:        0.89760E-01

===============================================================


 INSTANT    0.945000000E+03   TIME STEP NUMBER             945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998704E+04
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 :  0.23759E+00 0.12132E+01
   Friction velocity        uet   :  0.14220E-01 0.72309E-01
   Friction velocity        uk    :  0.17457E-01 0.38523E-01
   Dimensionless distance   yplus :  0.42848E+03 0.94372E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63873E+01      56   0.13879E-02   0.20946E-01 
c  VelocityX    0.46304E+04      12   0.71269E-02   0.39688E-03 
c  VelocityY    0.46304E+04      12   0.71269E-02   0.28610E-04 
c  VelocityZ    0.46304E+04      12   0.71269E-02   0.37503E-04 
c  TurbEner     0.59784E+01      13   0.77968E-04   0.11102E-08 
c  Dissip       0.14311E+01      16   0.12380E-02   0.27955E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.59           54516           26777           27271
v  Velocity[x]            0.29299          2.1986         0.90807         0.90984
v  Velocity[y]           -0.36805         0.70732      0.00056008      0.00033538
v  Velocity[z]           -0.42048         0.50503      -0.0012384       -0.001359
v  TurbEner             0.0010173        0.015347       0.0032863       0.0033454
v  Dissip              9.2111e-05         0.02941       0.0004506      0.00038964
v  TurbVisc               0.16592          11.371          4.7147          5.2757
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              945:        0.89886E-01

===============================================================


 INSTANT    0.946000000E+03   TIME STEP NUMBER             946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002288E+04
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 :  0.23759E+00 0.13245E+01
   Friction velocity        uet   :  0.14221E-01 0.78944E-01
   Friction velocity        uk    :  0.17470E-01 0.38585E-01
   Dimensionless distance   yplus :  0.42909E+03 0.94376E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62392E+01      55   0.13993E-02   0.20457E-01 
c  VelocityX    0.46303E+04      12   0.75443E-02   0.42297E-03 
c  VelocityY    0.46303E+04      12   0.75443E-02   0.23167E-04 
c  VelocityZ    0.46303E+04      12   0.75443E-02   0.49622E-04 
c  TurbEner     0.59786E+01      13   0.12809E-03   0.17722E-08 
c  Dissip       0.14570E+01      16   0.23255E-02   0.67221E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.55           54508           26777           27272
v  Velocity[x]            0.29273          2.0211         0.90808         0.90985
v  Velocity[y]           -0.38273         0.69858       0.0005566      0.00033557
v  Velocity[z]           -0.42196         0.51232      -0.0012554      -0.0013775
v  TurbEner             0.0010232        0.015991       0.0032866       0.0033456
v  Dissip              9.2117e-05        0.031283      0.00045098       0.0003899
v  TurbVisc               0.16639          11.345          4.7148          5.2758
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              946:        0.89359E-01

===============================================================


 INSTANT    0.947000000E+03   TIME STEP NUMBER             947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001240E+04
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 :  0.23774E+00 0.12158E+01
   Friction velocity        uet   :  0.14229E-01 0.72464E-01
   Friction velocity        uk    :  0.17521E-01 0.38623E-01
   Dimensionless distance   yplus :  0.42938E+03 0.94373E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64127E+01      54   0.14906E-02   0.21030E-01 
c  VelocityX    0.46303E+04      12   0.63868E-02   0.40887E-03 
c  VelocityY    0.46303E+04      12   0.63868E-02   0.57621E-04 
c  VelocityZ    0.46303E+04      12   0.63868E-02   0.13353E-03 
c  TurbEner     0.59779E+01      14   0.13363E-03   0.21941E-08 
c  Dissip       0.14380E+01      16   0.16439E-02   0.45116E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.87           54521           26777           27271
v  Velocity[x]            0.29302          2.0949         0.90805         0.90983
v  Velocity[y]           -0.36675         0.70561      0.00056926      0.00034442
v  Velocity[z]           -0.42112         0.50642      -0.0012353      -0.0013586
v  TurbEner             0.0010305        0.015409       0.0032868       0.0033458
v  Dissip              9.2124e-05        0.030234      0.00045102      0.00038992
v  TurbVisc               0.16679          11.336          4.7149          5.2759
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              947:        0.89606E-01

===============================================================


 INSTANT    0.948000000E+03   TIME STEP NUMBER             948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000835E+04
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 :  0.23777E+00 0.13251E+01
   Friction velocity        uet   :  0.14231E-01 0.78974E-01
   Friction velocity        uk    :  0.17583E-01 0.38593E-01
   Dimensionless distance   yplus :  0.43136E+03 0.94421E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58186E+01      64   0.14600E-02   0.19097E-01 
c  VelocityX    0.46303E+04      12   0.65547E-02   0.31097E-03 
c  VelocityY    0.46303E+04      12   0.65547E-02   0.31935E-04 
c  VelocityZ    0.46303E+04      12   0.65547E-02   0.55917E-04 
c  TurbEner     0.59782E+01      12   0.64578E-04   0.85798E-09 
c  Dissip       0.14524E+01      14   0.46077E-03   0.62227E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.06           54512           26779           27273
v  Velocity[x]            0.29259          2.1431         0.90807         0.90985
v  Velocity[y]           -0.38232         0.69834      0.00056584      0.00034533
v  Velocity[z]           -0.42103         0.51141      -0.0012343      -0.0013564
v  TurbEner             0.0010313        0.015325       0.0032869       0.0033459
v  Dissip              9.2108e-05        0.030287      0.00045118      0.00039003
v  TurbVisc               0.16804           11.37          4.7151           5.276
v  total_pressure           83076      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              948:        0.91738E-01

===============================================================


 INSTANT    0.949000000E+03   TIME STEP NUMBER             949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997551E+04
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 :  0.23775E+00 0.12296E+01
   Friction velocity        uet   :  0.14231E-01 0.72316E-01
   Friction velocity        uk    :  0.17589E-01 0.38496E-01
   Dimensionless distance   yplus :  0.43184E+03 0.94422E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59858E+01      58   0.12174E-02   0.19619E-01 
c  VelocityX    0.46303E+04      12   0.70666E-02   0.36318E-03 
c  VelocityY    0.46303E+04      12   0.70666E-02   0.24505E-04 
c  VelocityZ    0.46303E+04      12   0.70666E-02   0.33241E-04 
c  TurbEner     0.59788E+01      12   0.64650E-04   0.86130E-09 
c  Dissip       0.14811E+01      15   0.92920E-03   0.20841E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.33           54515           26778           27272
v  Velocity[x]             0.2926          2.1825         0.90805         0.90982
v  Velocity[y]           -0.36705         0.70735       0.0005637      0.00034078
v  Velocity[z]           -0.42275          0.5049       -0.001244      -0.0013664
v  TurbEner             0.0010384        0.015353       0.0032871        0.003346
v  Dissip              9.2096e-05        0.030691      0.00045149      0.00039023
v  TurbVisc               0.16829          11.355          4.7151          5.2761
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              949:        0.90051E-01

===============================================================


 INSTANT    0.950000000E+03   TIME STEP NUMBER             950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000593E+04
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 :  0.23747E+00 0.13247E+01
   Friction velocity        uet   :  0.14214E-01 0.78955E-01
   Friction velocity        uk    :  0.17650E-01 0.38511E-01
   Dimensionless distance   yplus :  0.43249E+03 0.94518E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58155E+01      58   0.14897E-02   0.19064E-01 
c  VelocityX    0.46302E+04      12   0.73042E-02   0.40076E-03 
c  VelocityY    0.46302E+04      12   0.73042E-02   0.21813E-04 
c  VelocityZ    0.46302E+04      12   0.73042E-02   0.40016E-04 
c  TurbEner     0.59792E+01      13   0.10787E-03   0.12049E-08 
c  Dissip       0.14987E+01      16   0.19852E-02   0.47441E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.72           54517           26778           27273
v  Velocity[x]            0.29292          2.0157         0.90806         0.90984
v  Velocity[y]            -0.3825         0.69829      0.00055753      0.00033755
v  Velocity[z]           -0.41891          0.5119      -0.0012457      -0.0013699
v  TurbEner             0.0010424        0.015847       0.0032873       0.0033462
v  Dissip              9.2051e-05        0.032274      0.00045184      0.00039048
v  TurbVisc               0.16874          11.362          4.7152          5.2762
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              950:        0.89501E-01

===============================================================


 INSTANT    0.951000000E+03   TIME STEP NUMBER             951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999534E+04
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 :  0.23752E+00 0.12163E+01
   Friction velocity        uet   :  0.14217E-01 0.72496E-01
   Friction velocity        uk    :  0.17684E-01 0.38587E-01
   Dimensionless distance   yplus :  0.43382E+03 0.94540E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66209E+01      61   0.16074E-02   0.21732E-01 
c  VelocityX    0.46303E+04      12   0.63653E-02   0.35759E-03 
c  VelocityY    0.46303E+04      12   0.63653E-02   0.46653E-04 
c  VelocityZ    0.46303E+04      12   0.63653E-02   0.69105E-04 
c  TurbEner     0.59777E+01      14   0.14434E-03   0.23960E-08 
c  Dissip       0.14686E+01      16   0.19983E-02   0.64593E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.55           54505           26778           27272
v  Velocity[x]            0.29265          2.0878         0.90805         0.90982
v  Velocity[y]           -0.36697         0.70531       0.0005712      0.00034731
v  Velocity[z]           -0.42047         0.50578      -0.0012435       -0.001365
v  TurbEner             0.0010428        0.015212       0.0032872       0.0033461
v  Dissip              9.2057e-05        0.031015      0.00045169      0.00039038
v  TurbVisc               0.16948          11.339          4.7152          5.2763
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              951:        0.89985E-01

===============================================================


 INSTANT    0.952000000E+03   TIME STEP NUMBER             952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001287E+04
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 :  0.23758E+00 0.13254E+01
   Friction velocity        uet   :  0.14221E-01 0.79000E-01
   Friction velocity        uk    :  0.17687E-01 0.38645E-01
   Dimensionless distance   yplus :  0.43432E+03 0.94567E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59702E+01      53   0.12776E-02   0.19574E-01 
c  VelocityX    0.46302E+04      12   0.68379E-02   0.35975E-03 
c  VelocityY    0.46302E+04      12   0.68379E-02   0.30007E-04 
c  VelocityZ    0.46302E+04      12   0.68379E-02   0.60728E-04 
c  TurbEner     0.59771E+01      13   0.63226E-04   0.85615E-09 
c  Dissip       0.14782E+01      14   0.42167E-03   0.38656E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.29           54509           26778           27272
v  Velocity[x]             0.2927          2.1399         0.90807         0.90984
v  Velocity[y]           -0.38294         0.69893      0.00055752      0.00033614
v  Velocity[z]           -0.42021         0.51048      -0.0012478      -0.0013714
v  TurbEner             0.0010458        0.015088        0.003287        0.003346
v  Dissip              9.2032e-05        0.030854      0.00045174      0.00039041
v  TurbVisc               0.16964           11.34          4.7152          5.2762
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              952:        0.88942E-01

===============================================================


 INSTANT    0.953000000E+03   TIME STEP NUMBER             953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001046E+04
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 :  0.23808E+00 0.12511E+01
   Friction velocity        uet   :  0.14250E-01 0.72963E-01
   Friction velocity        uk    :  0.17713E-01 0.38639E-01
   Dimensionless distance   yplus :  0.43417E+03 0.94535E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72020E+01      59   0.14551E-02   0.23596E-01 
c  VelocityX    0.46302E+04      12   0.72999E-02   0.34940E-03 
c  VelocityY    0.46302E+04      12   0.72999E-02   0.29976E-04 
c  VelocityZ    0.46302E+04      12   0.72999E-02   0.88583E-04 
c  TurbEner     0.59784E+01      12   0.71589E-04   0.72656E-09 
c  Dissip       0.15020E+01      15   0.69647E-03   0.12241E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.53           54527           26777           27271
v  Velocity[x]             0.2927          2.1862         0.90805         0.90982
v  Velocity[y]           -0.36739         0.70749      0.00056435      0.00033882
v  Velocity[z]           -0.42107         0.50438       -0.001229      -0.0013516
v  TurbEner             0.0010486        0.015108       0.0032871       0.0033461
v  Dissip               9.209e-05        0.031029      0.00045194      0.00039054
v  TurbVisc               0.16957          11.317          4.7151          5.2762
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              953:        0.90211E-01

===============================================================


 INSTANT    0.954000000E+03   TIME STEP NUMBER             954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002757E+04
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 :  0.23759E+00 0.13249E+01
   Friction velocity        uet   :  0.14221E-01 0.78975E-01
   Friction velocity        uk    :  0.17737E-01 0.38583E-01
   Dimensionless distance   yplus :  0.43535E+03 0.94490E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69334E+01      64   0.16047E-02   0.22753E-01 
c  VelocityX    0.46301E+04      12   0.64783E-02   0.46845E-03 
c  VelocityY    0.46301E+04      12   0.64783E-02   0.43277E-04 
c  VelocityZ    0.46301E+04      12   0.64783E-02   0.46947E-04 
c  TurbEner     0.59787E+01      13   0.12141E-03   0.15198E-08 
c  Dissip       0.15123E+01      16   0.19754E-02   0.43871E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.59           54507           26777           27272
v  Velocity[x]            0.29279          2.0113         0.90807         0.90985
v  Velocity[y]           -0.38227         0.69744      0.00055765      0.00033656
v  Velocity[z]            -0.4218         0.51191      -0.0012386      -0.0013612
v  TurbEner              0.001045        0.015698       0.0032872       0.0033462
v  Dissip              9.2103e-05        0.032595      0.00045221      0.00039075
v  TurbVisc               0.17021          11.298          4.7151          5.2763
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              954:        0.90794E-01

===============================================================


 INSTANT    0.955000000E+03   TIME STEP NUMBER             955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999098E+04
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 :  0.23760E+00 0.12180E+01
   Friction velocity        uet   :  0.14222E-01 0.72601E-01
   Friction velocity        uk    :  0.17706E-01 0.38520E-01
   Dimensionless distance   yplus :  0.43502E+03 0.94469E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59994E+01      55   0.11823E-02   0.19678E-01 
c  VelocityX    0.46302E+04      12   0.63200E-02   0.31189E-03 
c  VelocityY    0.46302E+04      12   0.63200E-02   0.41067E-04 
c  VelocityZ    0.46302E+04      12   0.63200E-02   0.29985E-04 
c  TurbEner     0.59768E+01      14   0.14957E-03   0.24563E-08 
c  Dissip       0.14809E+01      16   0.22049E-02   0.68255E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.22           54509           26777           27271
v  Velocity[x]            0.29286          2.1046         0.90804          0.9098
v  Velocity[y]           -0.36611         0.70584      0.00056184      0.00033755
v  Velocity[z]           -0.42148         0.50654      -0.0012359      -0.0013589
v  TurbEner             0.0010478         0.01499       0.0032869        0.003346
v  Dissip              9.2097e-05        0.031092      0.00045196      0.00039057
v  TurbVisc               0.16991          11.335          4.7151          5.2763
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              955:        0.89842E-01

===============================================================


 INSTANT    0.956000000E+03   TIME STEP NUMBER             956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001090E+04
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 :  0.23785E+00 0.13244E+01
   Friction velocity        uet   :  0.14236E-01 0.78939E-01
   Friction velocity        uk    :  0.17730E-01 0.38579E-01
   Dimensionless distance   yplus :  0.43488E+03 0.94475E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68836E+01      56   0.14299E-02   0.22562E-01 
c  VelocityX    0.46300E+04      12   0.73443E-02   0.31472E-03 
c  VelocityY    0.46300E+04      12   0.73443E-02   0.28863E-04 
c  VelocityZ    0.46300E+04      12   0.73443E-02   0.40207E-04 
c  TurbEner     0.59769E+01      12   0.60023E-04   0.51526E-09 
c  Dissip       0.14864E+01      13   0.30441E-03   0.20068E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.19           54522           26777           27271
v  Velocity[x]            0.29278          2.1432         0.90805         0.90983
v  Velocity[y]           -0.38224         0.70093      0.00054869      0.00032915
v  Velocity[z]           -0.41926         0.51114      -0.0012453      -0.0013672
v  TurbEner             0.0010478        0.014924       0.0032868       0.0033459
v  Dissip              9.2054e-05        0.030973      0.00045191      0.00039053
v  TurbVisc               0.16986          11.326           4.715          5.2762
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              956:        0.89109E-01

===============================================================


 INSTANT    0.957000000E+03   TIME STEP NUMBER             957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998560E+04
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 :  0.23741E+00 0.12341E+01
   Friction velocity        uet   :  0.14210E-01 0.72394E-01
   Friction velocity        uk    :  0.17730E-01 0.38638E-01
   Dimensionless distance   yplus :  0.43543E+03 0.94483E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64342E+01      59   0.12833E-02   0.21100E-01 
c  VelocityX    0.46302E+04      13   0.69127E-02   0.37541E-03 
c  VelocityY    0.46302E+04      13   0.69127E-02   0.27229E-04 
c  VelocityZ    0.46302E+04      13   0.69127E-02   0.10519E-03 
c  TurbEner     0.59776E+01      12   0.74811E-04   0.84987E-09 
c  Dissip       0.15109E+01      15   0.81287E-03   0.13698E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.67           54535           26776           27270
v  Velocity[x]            0.29261           2.179         0.90807         0.90984
v  Velocity[y]           -0.36768         0.70978      0.00055871      0.00033262
v  Velocity[z]           -0.41994         0.50419       -0.001244      -0.0013669
v  TurbEner             0.0010442        0.015089       0.0032867       0.0033458
v  Dissip              9.2029e-05        0.031399      0.00045204      0.00039061
v  TurbVisc               0.17013          11.324           4.715          5.2762
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              957:        0.90848E-01

===============================================================


 INSTANT    0.958000000E+03   TIME STEP NUMBER             958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000739E+04
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 :  0.23783E+00 0.13254E+01
   Friction velocity        uet   :  0.14236E-01 0.79000E-01
   Friction velocity        uk    :  0.17699E-01 0.38630E-01
   Dimensionless distance   yplus :  0.43517E+03 0.94515E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63136E+01      57   0.13580E-02   0.20693E-01 
c  VelocityX    0.46301E+04      12   0.73707E-02   0.37244E-03 
c  VelocityY    0.46301E+04      12   0.73707E-02   0.26227E-04 
c  VelocityZ    0.46301E+04      12   0.73707E-02   0.49668E-04 
c  TurbEner     0.59786E+01      13   0.75788E-04   0.91704E-09 
c  Dissip       0.15370E+01      15   0.94580E-03   0.18528E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -168.8           54547           26777           27271
v  Velocity[x]            0.29275          2.2007         0.90807         0.90985
v  Velocity[y]           -0.38237         0.69791      0.00054874      0.00032598
v  Velocity[z]           -0.42088         0.51172      -0.0012501      -0.0013713
v  TurbEner             0.0010441        0.015266       0.0032868       0.0033459
v  Dissip              9.2006e-05        0.031926      0.00045229      0.00039079
v  TurbVisc               0.16984          11.358           4.715          5.2761
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              958:        0.90073E-01

===============================================================


 INSTANT    0.959000000E+03   TIME STEP NUMBER             959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998686E+04
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 :  0.23795E+00 0.12190E+01
   Friction velocity        uet   :  0.14243E-01 0.72646E-01
   Friction velocity        uk    :  0.17699E-01 0.38633E-01
   Dimensionless distance   yplus :  0.43431E+03 0.94583E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73566E+01      54   0.16798E-02   0.24113E-01 
c  VelocityX    0.46301E+04      12   0.67992E-02   0.42049E-03 
c  VelocityY    0.46301E+04      12   0.67992E-02   0.48946E-04 
c  VelocityZ    0.46301E+04      12   0.67992E-02   0.29144E-04 
c  TurbEner     0.59795E+01      13   0.12083E-03   0.14631E-08 
c  Dissip       0.15583E+01      16   0.21136E-02   0.52781E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.92           54538           26776           27270
v  Velocity[x]            0.29295           2.042         0.90806         0.90983
v  Velocity[y]           -0.36652         0.70683      0.00055919      0.00033632
v  Velocity[z]           -0.42192         0.50608      -0.0012475      -0.0013701
v  TurbEner             0.0010447        0.015823        0.003287        0.003346
v  Dissip               9.206e-05        0.033614      0.00045262      0.00039104
v  TurbVisc               0.16934          11.339          4.7149           5.276
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              959:        0.89836E-01

===============================================================


 INSTANT    0.960000000E+03   TIME STEP NUMBER             960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001793E+04
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 :  0.23734E+00 0.13250E+01
   Friction velocity        uet   :  0.14206E-01 0.78961E-01
   Friction velocity        uk    :  0.17704E-01 0.38631E-01
   Dimensionless distance   yplus :  0.43496E+03 0.94590E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71948E+01      60   0.17137E-02   0.23599E-01 
c  VelocityX    0.46300E+04      12   0.65931E-02   0.35992E-03 
c  VelocityY    0.46300E+04      12   0.65931E-02   0.47862E-04 
c  VelocityZ    0.46300E+04      12   0.65931E-02   0.49584E-04 
c  TurbEner     0.59783E+01      13   0.13568E-03   0.21683E-08 
c  Dissip       0.15284E+01      16   0.19665E-02   0.58879E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -171.27           54515           26777           27271
v  Velocity[x]            0.29261          2.0981         0.90807         0.90984
v  Velocity[y]           -0.38224         0.70222      0.00055022      0.00033121
v  Velocity[z]           -0.42072           0.511      -0.0012417       -0.001364
v  TurbEner             0.0010386        0.015238       0.0032869        0.003346
v  Dissip              9.2021e-05        0.032303      0.00045248      0.00039096
v  TurbVisc               0.16964          11.339          4.7148           5.276
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              960:        0.90388E-01

===============================================================


 INSTANT    0.961000000E+03   TIME STEP NUMBER             961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999501E+04
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 :  0.23791E+00 0.12204E+01
   Friction velocity        uet   :  0.14241E-01 0.72616E-01
   Friction velocity        uk    :  0.17652E-01 0.38578E-01
   Dimensionless distance   yplus :  0.43407E+03 0.94625E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66154E+01      61   0.14261E-02   0.21691E-01 
c  VelocityX    0.46300E+04      12   0.68837E-02   0.35230E-03 
c  VelocityY    0.46300E+04      12   0.68837E-02   0.41124E-04 
c  VelocityZ    0.46300E+04      12   0.68837E-02   0.11277E-03 
c  TurbEner     0.59779E+01      13   0.70144E-04   0.95083E-09 
c  Dissip       0.15342E+01      13   0.30138E-03   0.20266E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.85           54526           26776           27270
v  Velocity[x]            0.29274           2.155         0.90803         0.90981
v  Velocity[y]           -0.36698         0.70978      0.00057114      0.00034607
v  Velocity[z]            -0.4219         0.50468      -0.0012402       -0.001363
v  TurbEner             0.0010388         0.01517       0.0032869        0.003346
v  Dissip               9.203e-05        0.032145      0.00045249      0.00039097
v  TurbVisc               0.16896          11.314          4.7146          5.2758
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              961:        0.90179E-01

===============================================================


 INSTANT    0.962000000E+03   TIME STEP NUMBER             962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001306E+04
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 :  0.23763E+00 0.13245E+01
   Friction velocity        uet   :  0.14224E-01 0.78943E-01
   Friction velocity        uk    :  0.17653E-01 0.38633E-01
   Dimensionless distance   yplus :  0.43338E+03 0.94583E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68185E+01      55   0.12718E-02   0.22353E-01 
c  VelocityX    0.46299E+04      12   0.67034E-02   0.37465E-03 
c  VelocityY    0.46299E+04      12   0.67034E-02   0.50240E-04 
c  VelocityZ    0.46299E+04      12   0.67034E-02   0.55199E-04 
c  TurbEner     0.59785E+01      13   0.70804E-04   0.10033E-08 
c  Dissip       0.15533E+01      15   0.82254E-03   0.17339E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -172.48           54532           26776           27270
v  Velocity[x]            0.29275          2.1801         0.90806         0.90984
v  Velocity[y]           -0.38246         0.70126      0.00055398      0.00033123
v  Velocity[z]           -0.41858         0.51174      -0.0012433      -0.0013635
v  TurbEner             0.0010367        0.015257       0.0032869        0.003346
v  Dissip               9.204e-05        0.032369      0.00045268      0.00039111
v  TurbVisc               0.16852          11.322          4.7146          5.2757
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              962:        0.89252E-01

===============================================================


 INSTANT    0.963000000E+03   TIME STEP NUMBER             963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000289E+04
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 :  0.23762E+00 0.12179E+01
   Friction velocity        uet   :  0.14223E-01 0.72589E-01
   Friction velocity        uk    :  0.17635E-01 0.38640E-01
   Dimensionless distance   yplus :  0.43341E+03 0.94574E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70851E+01      55   0.15787E-02   0.23234E-01 
c  VelocityX    0.46300E+04      12   0.66367E-02   0.32797E-03 
c  VelocityY    0.46300E+04      12   0.66367E-02   0.41642E-04 
c  VelocityZ    0.46300E+04      12   0.66367E-02   0.28159E-04 
c  TurbEner     0.59788E+01      13   0.10580E-03   0.10183E-08 
c  Dissip       0.15678E+01      16   0.18823E-02   0.40795E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -179           54539           26775           27270
v  Velocity[x]            0.29285          2.0321         0.90805         0.90982
v  Velocity[y]           -0.36691         0.70778      0.00055854      0.00033313
v  Velocity[z]           -0.42048         0.50569      -0.0012556      -0.0013761
v  TurbEner             0.0010312        0.015736       0.0032869        0.003346
v  Dissip              9.2091e-05         0.03386      0.00045291      0.00039128
v  TurbVisc               0.16844          11.338          4.7145          5.2756
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              963:        0.89744E-01

===============================================================


 INSTANT    0.964000000E+03   TIME STEP NUMBER             964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000880E+04
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 :  0.23763E+00 0.13262E+01
   Friction velocity        uet   :  0.14224E-01 0.79036E-01
   Friction velocity        uk    :  0.17588E-01 0.38608E-01
   Dimensionless distance   yplus :  0.43266E+03 0.94579E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64777E+01      53   0.12481E-02   0.21234E-01 
c  VelocityX    0.46299E+04      12   0.72516E-02   0.38190E-03 
c  VelocityY    0.46299E+04      12   0.72516E-02   0.26644E-04 
c  VelocityZ    0.46299E+04      12   0.72516E-02   0.37935E-04 
c  TurbEner     0.59776E+01      13   0.13940E-03   0.17775E-08 
c  Dissip       0.15331E+01      16   0.21579E-02   0.66935E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.28           54549           26776           27270
v  Velocity[x]            0.29292          2.0946         0.90807         0.90984
v  Velocity[y]           -0.38282         0.70218      0.00054069      0.00032039
v  Velocity[z]           -0.42183         0.51051      -0.0012533      -0.0013728
v  TurbEner              0.001029        0.015096       0.0032868       0.0033459
v  Dissip              9.2112e-05        0.032409      0.00045274      0.00039117
v  TurbVisc                0.1678          11.381          4.7143          5.2754
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              964:        0.89483E-01

===============================================================


 INSTANT    0.965000000E+03   TIME STEP NUMBER             965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999315E+04
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 :  0.23777E+00 0.12203E+01
   Friction velocity        uet   :  0.14232E-01 0.72377E-01
   Friction velocity        uk    :  0.17570E-01 0.38575E-01
   Dimensionless distance   yplus :  0.43139E+03 0.94506E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64351E+01      58   0.14916E-02   0.21083E-01 
c  VelocityX    0.46299E+04      12   0.71759E-02   0.37538E-03 
c  VelocityY    0.46299E+04      12   0.71759E-02   0.27965E-04 
c  VelocityZ    0.46299E+04      12   0.71759E-02   0.10031E-03 
c  TurbEner     0.59782E+01      13   0.72287E-04   0.88219E-09 
c  Dissip       0.15374E+01      13   0.32517E-03   0.21353E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.59           54539           26775           27269
v  Velocity[x]            0.29282           2.147         0.90805         0.90982
v  Velocity[y]           -0.36732         0.70943      0.00055879      0.00033525
v  Velocity[z]           -0.42083         0.50431      -0.0012378      -0.0013597
v  TurbEner              0.001028        0.015022       0.0032869        0.003346
v  Dissip              9.2069e-05        0.032241      0.00045277       0.0003912
v  TurbVisc                0.1671          11.359          4.7141          5.2752
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              965:        0.89954E-01

===============================================================


 INSTANT    0.966000000E+03   TIME STEP NUMBER             966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000698E+04
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 :  0.23770E+00 0.13259E+01
   Friction velocity        uet   :  0.14228E-01 0.79027E-01
   Friction velocity        uk    :  0.17561E-01 0.38614E-01
   Dimensionless distance   yplus :  0.43173E+03 0.94447E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61815E+01      63   0.15123E-02   0.20286E-01 
c  VelocityX    0.46299E+04      12   0.74546E-02   0.36577E-03 
c  VelocityY    0.46299E+04      12   0.74546E-02   0.28036E-04 
c  VelocityZ    0.46299E+04      12   0.74546E-02   0.54065E-04 
c  TurbEner     0.59790E+01      13   0.80746E-04   0.13673E-08 
c  Dissip       0.15525E+01      15   0.74446E-03   0.14492E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -170.74           54515           26777           27271
v  Velocity[x]             0.2926          2.1781         0.90807         0.90985
v  Velocity[y]            -0.3822         0.69986      0.00055254       0.0003303
v  Velocity[z]           -0.42186         0.51186       -0.001236      -0.0013559
v  TurbEner             0.0010208         0.01506       0.0032871       0.0033462
v  Dissip              9.2079e-05        0.032361      0.00045297      0.00039135
v  TurbVisc               0.16724          11.362           4.714          5.2751
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              966:        0.90771E-01

===============================================================


 INSTANT    0.967000000E+03   TIME STEP NUMBER             967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997722E+04
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 :  0.23775E+00 0.12386E+01
   Friction velocity        uet   :  0.14230E-01 0.72506E-01
   Friction velocity        uk    :  0.17500E-01 0.38555E-01
   Dimensionless distance   yplus :  0.43061E+03 0.94433E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70803E+01      58   0.15493E-02   0.23210E-01 
c  VelocityX    0.46298E+04      12   0.67534E-02   0.44328E-03 
c  VelocityY    0.46298E+04      12   0.67534E-02   0.40776E-04 
c  VelocityZ    0.46298E+04      12   0.67534E-02   0.31968E-04 
c  TurbEner     0.59787E+01      13   0.10427E-03   0.13227E-08 
c  Dissip       0.15638E+01      15   0.16803E-02   0.30969E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.43           54520           26775           27269
v  Velocity[x]            0.29281          2.0285         0.90804         0.90981
v  Velocity[y]           -0.36603         0.70654      0.00056252      0.00033932
v  Velocity[z]            -0.4225         0.50663      -0.0012474      -0.0013679
v  TurbEner             0.0010204        0.015518       0.0032872       0.0033462
v  Dissip              9.2097e-05        0.033686      0.00045313      0.00039148
v  TurbVisc                0.1664          11.335          4.7139          5.2749
v  total_pressure           83080      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              967:        0.89863E-01

===============================================================


 INSTANT    0.968000000E+03   TIME STEP NUMBER             968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001574E+04
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 :  0.23763E+00 0.13254E+01
   Friction velocity        uet   :  0.14222E-01 0.78989E-01
   Friction velocity        uk    :  0.17496E-01 0.38568E-01
   Dimensionless distance   yplus :  0.42974E+03 0.94368E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69331E+01      53   0.14036E-02   0.22722E-01 
c  VelocityX    0.46298E+04      12   0.72543E-02   0.39114E-03 
c  VelocityY    0.46298E+04      12   0.72543E-02   0.46996E-04 
c  VelocityZ    0.46298E+04      12   0.72543E-02   0.42198E-04 
c  TurbEner     0.59771E+01      13   0.15029E-03   0.22026E-08 
c  Dissip       0.15202E+01      17   0.25471E-02   0.90688E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.21           54521           26776           27270
v  Velocity[x]            0.29303          2.0905         0.90807         0.90984
v  Velocity[y]           -0.38222         0.70087      0.00054806      0.00032967
v  Velocity[z]           -0.41947         0.51113      -0.0012372      -0.0013592
v  TurbEner              0.001018        0.014881       0.0032869       0.0033461
v  Dissip              9.2072e-05        0.032003      0.00045285      0.00039128
v  TurbVisc               0.16606          11.325          4.7137          5.2748
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              968:        0.89399E-01

===============================================================


 INSTANT    0.969000000E+03   TIME STEP NUMBER             969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999595E+04
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 :  0.23746E+00 0.12227E+01
   Friction velocity        uet   :  0.14211E-01 0.72334E-01
   Friction velocity        uk    :  0.17476E-01 0.38569E-01
   Dimensionless distance   yplus :  0.42964E+03 0.94340E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64457E+01      56   0.15397E-02   0.21146E-01 
c  VelocityX    0.46299E+04      13   0.68431E-02   0.37372E-03 
c  VelocityY    0.46299E+04      13   0.68431E-02   0.34218E-04 
c  VelocityZ    0.46299E+04      13   0.68431E-02   0.58044E-04 
c  TurbEner     0.59773E+01      12   0.60534E-04   0.66118E-09 
c  Dissip       0.15159E+01      14   0.53285E-03   0.40184E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.83           54511           26775           27270
v  Velocity[x]            0.29281          2.1458         0.90805         0.90982
v  Velocity[y]           -0.36766         0.70868      0.00056614       0.0003446
v  Velocity[z]           -0.42012         0.50423      -0.0012354      -0.0013573
v  TurbEner             0.0010138        0.014824       0.0032868        0.003346
v  Dissip              9.2047e-05        0.031665      0.00045273       0.0003912
v  TurbVisc               0.16603           11.35          4.7135          5.2745
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              969:        0.89816E-01

===============================================================


 INSTANT    0.970000000E+03   TIME STEP NUMBER             970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000684E+04
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 :  0.23768E+00 0.13251E+01
   Friction velocity        uet   :  0.14223E-01 0.78976E-01
   Friction velocity        uk    :  0.17440E-01 0.38466E-01
   Dimensionless distance   yplus :  0.42911E+03 0.94382E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62595E+01      57   0.12559E-02   0.20523E-01 
c  VelocityX    0.46298E+04      12   0.68954E-02   0.31702E-03 
c  VelocityY    0.46298E+04      12   0.68954E-02   0.33864E-04 
c  VelocityZ    0.46298E+04      12   0.68954E-02   0.46222E-04 
c  TurbEner     0.59772E+01      13   0.76750E-04   0.13916E-08 
c  Dissip       0.15296E+01      15   0.68492E-03   0.12422E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.61           54514           26776           27270
v  Velocity[x]            0.29256          2.1754         0.90807         0.90984
v  Velocity[y]           -0.38246         0.69899       0.0005526      0.00033122
v  Velocity[z]           -0.42085         0.51181      -0.0012417      -0.0013634
v  TurbEner             0.0010141        0.014942       0.0032866       0.0033459
v  Dissip              9.2082e-05        0.031781      0.00045272      0.00039118
v  TurbVisc               0.16561          11.395          4.7133          5.2744
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              970:        0.89877E-01

===============================================================


 INSTANT    0.971000000E+03   TIME STEP NUMBER             971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997558E+04
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 :  0.23795E+00 0.12628E+01
   Friction velocity        uet   :  0.14238E-01 0.73669E-01
   Friction velocity        uk    :  0.17443E-01 0.38521E-01
   Dimensionless distance   yplus :  0.42828E+03 0.94352E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64467E+01      56   0.12974E-02   0.21119E-01 
c  VelocityX    0.46299E+04      12   0.79821E-02   0.34280E-03 
c  VelocityY    0.46299E+04      12   0.79821E-02   0.30759E-04 
c  VelocityZ    0.46299E+04      12   0.79821E-02   0.34146E-04 
c  TurbEner     0.59785E+01      12   0.77528E-04   0.84881E-09 
c  Dissip       0.15587E+01      15   0.83919E-03   0.13229E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.22           54528           26776           27270
v  Velocity[x]            0.29287          2.2087         0.90806         0.90983
v  Velocity[y]           -0.36646         0.70543      0.00055468      0.00032968
v  Velocity[z]           -0.42066         0.50607      -0.0012468      -0.0013676
v  TurbEner             0.0010159        0.015149       0.0032866       0.0033459
v  Dissip              9.2108e-05        0.032284      0.00045288      0.00039128
v  TurbVisc               0.16528          11.381          4.7131          5.2742
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              971:        0.89716E-01

===============================================================


 INSTANT    0.972000000E+03   TIME STEP NUMBER             972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000516E+04
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 :  0.23776E+00 0.13250E+01
   Friction velocity        uet   :  0.14225E-01 0.78960E-01
   Friction velocity        uk    :  0.17458E-01 0.38527E-01
   Dimensionless distance   yplus :  0.42912E+03 0.94400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64981E+01      55   0.15416E-02   0.21311E-01 
c  VelocityX    0.46298E+04      12   0.71678E-02   0.42747E-03 
c  VelocityY    0.46298E+04      12   0.71678E-02   0.29546E-04 
c  VelocityZ    0.46298E+04      12   0.71678E-02   0.10495E-03 
c  TurbEner     0.59791E+01      13   0.13034E-03   0.14420E-08 
c  Dissip       0.15755E+01      16   0.20929E-02   0.50275E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.02           54540           26776           27270
v  Velocity[x]            0.29272          2.0387         0.90807         0.90984
v  Velocity[y]           -0.38216         0.69849      0.00055306      0.00032887
v  Velocity[z]           -0.42229         0.51111      -0.0012419      -0.0013644
v  TurbEner             0.0010115        0.015779       0.0032866       0.0033459
v  Dissip              9.2119e-05        0.033952      0.00045306      0.00039142
v  TurbVisc               0.16573          11.328           4.713          5.2741
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              972:        0.89012E-01

===============================================================


 INSTANT    0.973000000E+03   TIME STEP NUMBER             973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999581E+04
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 :  0.23766E+00 0.12129E+01
   Friction velocity        uet   :  0.14219E-01 0.72287E-01
   Friction velocity        uk    :  0.17420E-01 0.38471E-01
   Dimensionless distance   yplus :  0.42849E+03 0.94444E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.70299E+01      54   0.13733E-02   0.23042E-01 
c  VelocityX    0.46297E+04      12   0.67755E-02   0.47814E-03 
c  VelocityY    0.46297E+04      12   0.67755E-02   0.23785E-04 
c  VelocityZ    0.46297E+04      12   0.67755E-02   0.61598E-04 
c  TurbEner     0.59772E+01      14   0.12250E-03   0.22473E-08 
c  Dissip       0.15247E+01      16   0.15923E-02   0.63167E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.58           54546           26775           27269
v  Velocity[x]            0.29281          1.7337         0.90805         0.90982
v  Velocity[y]           -0.36687         0.70697      0.00054822      0.00032588
v  Velocity[z]           -0.42205         0.50477      -0.0012548      -0.0013742
v  TurbEner             0.0010137        0.015635       0.0032863       0.0033456
v  Dissip              9.2129e-05        0.033913      0.00045278      0.00039125
v  TurbVisc               0.16517          11.319          4.7128           5.274
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              973:        0.89369E-01

===============================================================


 INSTANT    0.974000000E+03   TIME STEP NUMBER             974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001559E+04
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 :  0.23791E+00 0.13241E+01
   Friction velocity        uet   :  0.14233E-01 0.78923E-01
   Friction velocity        uk    :  0.17439E-01 0.38532E-01
   Dimensionless distance   yplus :  0.42811E+03 0.94466E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57161E+01      51   0.13218E-02   0.18739E-01 
c  VelocityX    0.46296E+04      12   0.65980E-02   0.37165E-03 
c  VelocityY    0.46296E+04      12   0.65980E-02   0.25909E-04 
c  VelocityZ    0.46296E+04      12   0.65980E-02   0.25860E-04 
c  TurbEner     0.59727E+01      15   0.41930E-03   0.97429E-08 
c  Dissip       0.13740E+01      18   0.81800E-02   0.48503E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.05           54540           26776           27270
v  Velocity[x]              0.293          1.8795         0.90804         0.90982
v  Velocity[y]            -0.3824         0.69762      0.00055877      0.00033933
v  Velocity[z]           -0.41952         0.51171      -0.0012472       -0.001368
v  TurbEner             0.0010133        0.013408        0.003286       0.0033454
v  Dissip              9.2131e-05        0.028252      0.00045203      0.00039069
v  TurbVisc               0.16499          11.349          4.7126          5.2738
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              974:        0.89201E-01

===============================================================


 INSTANT    0.975000000E+03   TIME STEP NUMBER             975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999319E+04
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 :  0.23739E+00 0.12153E+01
   Friction velocity        uet   :  0.14201E-01 0.72437E-01
   Friction velocity        uk    :  0.17435E-01 0.38568E-01
   Dimensionless distance   yplus :  0.42847E+03 0.94415E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59225E+01      66   0.15131E-02   0.19433E-01 
c  VelocityX    0.46298E+04      12   0.66331E-02   0.38983E-03 
c  VelocityY    0.46298E+04      12   0.66331E-02   0.26667E-04 
c  VelocityZ    0.46298E+04      12   0.66331E-02   0.34487E-04 
c  TurbEner     0.59710E+01      14   0.17288E-03   0.32335E-08 
c  Dissip       0.13174E+01      18   0.38313E-02   0.13722E-07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -178.35           54517           26775           27270
v  Velocity[x]            0.29281          1.9987         0.90805         0.90983
v  Velocity[y]           -0.36688         0.70549      0.00056977       0.0003477
v  Velocity[z]           -0.42009         0.50573      -0.0012375      -0.0013559
v  TurbEner             0.0010097        0.012628       0.0032854        0.003345
v  Dissip              9.2149e-05         0.02584      0.00045129      0.00039018
v  TurbVisc                0.1651          11.334          4.7126          5.2738
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              975:        0.92338E-01

===============================================================


 INSTANT    0.976000000E+03   TIME STEP NUMBER             976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999508E+04
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 :  0.23782E+00 0.13242E+01
   Friction velocity        uet   :  0.14226E-01 0.78925E-01
   Friction velocity        uk    :  0.17404E-01 0.38563E-01
   Dimensionless distance   yplus :  0.42809E+03 0.94448E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56620E+01      57   0.12008E-02   0.18565E-01 
c  VelocityX    0.46297E+04      12   0.65873E-02   0.36962E-03 
c  VelocityY    0.46297E+04      12   0.65873E-02   0.22844E-04 
c  VelocityZ    0.46297E+04      12   0.65873E-02   0.33943E-04 
c  TurbEner     0.59696E+01      13   0.10352E-03   0.19024E-08 
c  Dissip       0.12806E+01      18   0.24312E-02   0.87005E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.91           54526           26776           27271
v  Velocity[x]            0.29265          2.0764         0.90805         0.90982
v  Velocity[y]           -0.38288         0.70035      0.00056064      0.00033978
v  Velocity[z]           -0.42084         0.51044      -0.0012462      -0.0013683
v  TurbEner             0.0010094         0.01246       0.0032849       0.0033447
v  Dissip              9.2131e-05        0.024765       0.0004505      0.00038964
v  TurbVisc               0.16459          11.344          4.7124          5.2736
v  total_pressure           83075      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              976:        0.89888E-01

===============================================================


 INSTANT    0.977000000E+03   TIME STEP NUMBER             977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998954E+04
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 :  0.23794E+00 0.12132E+01
   Friction velocity        uet   :  0.14233E-01 0.72310E-01
   Friction velocity        uk    :  0.17402E-01 0.38571E-01
   Dimensionless distance   yplus :  0.42725E+03 0.94465E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64742E+01      62   0.13322E-02   0.21213E-01 
c  VelocityX    0.46298E+04      12   0.69742E-02   0.32459E-03 
c  VelocityY    0.46298E+04      12   0.69742E-02   0.35570E-04 
c  VelocityZ    0.46298E+04      12   0.69742E-02   0.31302E-04 
c  TurbEner     0.59695E+01      13   0.75077E-04   0.99610E-09 
c  Dissip       0.12696E+01      17   0.11316E-02   0.25960E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.87           54533           26775           27269
v  Velocity[x]            0.29308          2.1362         0.90803         0.90981
v  Velocity[y]           -0.36738         0.70806      0.00056196      0.00034024
v  Velocity[z]           -0.42171         0.50421      -0.0012411       -0.001359
v  TurbEner             0.0010095        0.012634       0.0032844       0.0033443
v  Dissip              9.2107e-05        0.024485      0.00044983      0.00038918
v  TurbVisc               0.16424          11.384          4.7124          5.2736
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              977:        0.90647E-01

===============================================================


 INSTANT    0.978000000E+03   TIME STEP NUMBER             978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002384E+04
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 :  0.23757E+00 0.13251E+01
   Friction velocity        uet   :  0.14210E-01 0.78983E-01
   Friction velocity        uk    :  0.17402E-01 0.38609E-01
   Dimensionless distance   yplus :  0.42780E+03 0.94529E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61739E+01      55   0.13448E-02   0.20250E-01 
c  VelocityX    0.46298E+04      12   0.64635E-02   0.32986E-03 
c  VelocityY    0.46298E+04      12   0.64635E-02   0.47570E-04 
c  VelocityZ    0.46298E+04      12   0.64635E-02   0.31743E-04 
c  TurbEner     0.59700E+01      13   0.13109E-03   0.18808E-08 
c  Dissip       0.12654E+01      17   0.15306E-02   0.24779E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.75           54541           26776           27270
v  Velocity[x]            0.29258          1.9795         0.90806         0.90983
v  Velocity[y]           -0.38228         0.69742      0.00055695      0.00033528
v  Velocity[z]           -0.42066         0.51186      -0.0012513       -0.001372
v  TurbEner             0.0010042        0.013336       0.0032842       0.0033442
v  Dissip              9.2083e-05        0.025481      0.00044939      0.00038889
v  TurbVisc               0.16452           11.36          4.7123          5.2736
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              978:        0.89997E-01

===============================================================


 INSTANT    0.979000000E+03   TIME STEP NUMBER             979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998392E+04
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 :  0.23796E+00 0.12172E+01
   Friction velocity        uet   :  0.14234E-01 0.72552E-01
   Friction velocity        uk    :  0.17357E-01 0.38571E-01
   Dimensionless distance   yplus :  0.42705E+03 0.94619E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61605E+01      60   0.12749E-02   0.20192E-01 
c  VelocityX    0.46298E+04      12   0.73624E-02   0.33064E-03 
c  VelocityY    0.46298E+04      12   0.73624E-02   0.30674E-04 
c  VelocityZ    0.46298E+04      12   0.73624E-02   0.51719E-04 
c  TurbEner     0.59695E+01      13   0.80717E-04   0.95108E-09 
c  Dissip       0.12339E+01      17   0.21651E-02   0.64806E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.66           54549           26776           27270
v  Velocity[x]            0.29239          2.0669         0.90805         0.90982
v  Velocity[y]           -0.36605         0.70594      0.00055864      0.00033506
v  Velocity[z]           -0.42185         0.50653      -0.0012485      -0.0013674
v  TurbEner             0.0010057        0.013086       0.0032838       0.0033439
v  Dissip              9.2037e-05        0.024327      0.00044873      0.00038843
v  TurbVisc                0.1639          11.363          4.7124          5.2736
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1998e+05


 TIME FOR THE TIME STEP              979:        0.89761E-01

===============================================================


 INSTANT    0.980000000E+03   TIME STEP NUMBER             980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999301E+04
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 :  0.23771E+00 0.13241E+01
   Friction velocity        uet   :  0.14219E-01 0.78914E-01
   Friction velocity        uk    :  0.17369E-01 0.38615E-01
   Dimensionless distance   yplus :  0.42659E+03 0.94613E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62961E+01      56   0.14368E-02   0.20631E-01 
c  VelocityX    0.46298E+04      12   0.71057E-02   0.36061E-03 
c  VelocityY    0.46298E+04      12   0.71057E-02   0.26191E-04 
c  VelocityZ    0.46298E+04      12   0.71057E-02   0.84563E-04 
c  TurbEner     0.59706E+01      13   0.71942E-04   0.94215E-09 
c  Dissip       0.12356E+01      15   0.50523E-03   0.50920E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -169.5           54541           26776           27270
v  Velocity[x]            0.29316          2.1242         0.90806         0.90984
v  Velocity[y]            -0.3822         0.70154      0.00056151      0.00033988
v  Velocity[z]           -0.41855          0.5111      -0.0012406      -0.0013623
v  TurbEner             0.0010049        0.013256       0.0032838       0.0033439
v  Dissip              9.2052e-05        0.024106      0.00044841      0.00038822
v  TurbVisc               0.16387          11.334          4.7124          5.2736
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              980:        0.89503E-01

===============================================================


 INSTANT    0.981000000E+03   TIME STEP NUMBER             981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997709E+04
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 :  0.23761E+00 0.12482E+01
   Friction velocity        uet   :  0.14213E-01 0.72864E-01
   Friction velocity        uk    :  0.17363E-01 0.38648E-01
   Dimensionless distance   yplus :  0.42691E+03 0.94629E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63113E+01      65   0.14847E-02   0.20701E-01 
c  VelocityX    0.46300E+04      13   0.68530E-02   0.40319E-03 
c  VelocityY    0.46300E+04      13   0.68530E-02   0.26054E-04 
c  VelocityZ    0.46300E+04      13   0.68530E-02   0.43793E-04 
c  TurbEner     0.59722E+01      13   0.10970E-03   0.19414E-08 
c  Dissip       0.12562E+01      16   0.10962E-02   0.20954E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -175.67           54516           26777           27271
v  Velocity[x]            0.29267          2.1634         0.90806         0.90984
v  Velocity[y]           -0.36764         0.71005      0.00056548      0.00034283
v  Velocity[z]           -0.42031         0.50419      -0.0012395      -0.0013583
v  TurbEner             0.0010011        0.013699       0.0032839        0.003344
v  Dissip              9.2124e-05        0.024692      0.00044834      0.00038819
v  TurbVisc               0.16409          11.332          4.7126          5.2738
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              981:        0.92511E-01

===============================================================


 INSTANT    0.982000000E+03   TIME STEP NUMBER             982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998697E+04
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 :  0.23763E+00 0.13255E+01
   Friction velocity        uet   :  0.14214E-01 0.78998E-01
   Friction velocity        uk    :  0.17330E-01 0.38597E-01
   Dimensionless distance   yplus :  0.42648E+03 0.94642E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58652E+01      53   0.13089E-02   0.19229E-01 
c  VelocityX    0.46299E+04      12   0.67872E-02   0.36599E-03 
c  VelocityY    0.46299E+04      12   0.67872E-02   0.26838E-04 
c  VelocityZ    0.46299E+04      12   0.67872E-02   0.46252E-04 
c  TurbEner     0.59732E+01      14   0.11298E-03   0.21841E-08 
c  Dissip       0.12863E+01      16   0.13357E-02   0.30624E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.28           54524           26777           27271
v  Velocity[x]            0.29248          2.1884         0.90805         0.90983
v  Velocity[y]           -0.38245         0.69766      0.00055683      0.00033354
v  Velocity[z]           -0.42177         0.51167      -0.0012464      -0.0013663
v  TurbEner             0.0010009        0.014133       0.0032842       0.0033442
v  Dissip              9.2143e-05        0.025476      0.00044846      0.00038828
v  TurbVisc               0.16371           11.37          4.7128           5.274
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              982:        0.89119E-01

===============================================================


 INSTANT    0.983000000E+03   TIME STEP NUMBER             983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000284E+04
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 :  0.23786E+00 0.12192E+01
   Friction velocity        uet   :  0.14228E-01 0.72652E-01
   Friction velocity        uk    :  0.17329E-01 0.38628E-01
   Dimensionless distance   yplus :  0.42554E+03 0.94583E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.68291E+01      53   0.14640E-02   0.22386E-01 
c  VelocityX    0.46300E+04      12   0.72632E-02   0.36821E-03 
c  VelocityY    0.46300E+04      12   0.72632E-02   0.42780E-04 
c  VelocityZ    0.46300E+04      12   0.72632E-02   0.38742E-04 
c  TurbEner     0.59746E+01      14   0.15044E-03   0.24791E-08 
c  Dissip       0.13143E+01      17   0.24246E-02   0.68604E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.35           54534           26777           27271
v  Velocity[x]            0.29302          2.0271         0.90805         0.90982
v  Velocity[y]           -0.36658         0.70733      0.00057153      0.00034583
v  Velocity[z]           -0.42088         0.50601      -0.0012527      -0.0013699
v  TurbEner             0.0010018        0.014955       0.0032844       0.0033443
v  Dissip              9.2098e-05        0.027311      0.00044873      0.00038848
v  TurbVisc               0.16343          11.354           4.713          5.2742
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              983:        0.89480E-01

===============================================================


 INSTANT    0.984000000E+03   TIME STEP NUMBER             984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999617E+04
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 :  0.23784E+00 0.13239E+01
   Friction velocity        uet   :  0.14227E-01 0.78891E-01
   Friction velocity        uk    :  0.17336E-01 0.38660E-01
   Dimensionless distance   yplus :  0.42624E+03 0.94562E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65174E+01      54   0.13393E-02   0.21380E-01 
c  VelocityX    0.46300E+04      12   0.68843E-02   0.33530E-03 
c  VelocityY    0.46300E+04      12   0.68843E-02   0.40059E-04 
c  VelocityZ    0.46300E+04      12   0.68843E-02   0.38350E-04 
c  TurbEner     0.59744E+01      14   0.97196E-04   0.16118E-08 
c  Dissip       0.13039E+01      16   0.12109E-02   0.23589E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.55           54543           26778           27272
v  Velocity[x]            0.29289          2.0907         0.90808         0.90985
v  Velocity[y]           -0.38226         0.70071      0.00055536      0.00033255
v  Velocity[z]           -0.42087         0.51106      -0.0012608      -0.0013802
v  TurbEner            0.00099682         0.01459       0.0032847       0.0033445
v  Dissip              9.2093e-05        0.026562      0.00044869      0.00038845
v  TurbVisc               0.16391          11.357          4.7132          5.2743
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              984:        0.89800E-01

===============================================================


 INSTANT    0.985000000E+03   TIME STEP NUMBER             985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998459E+04
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 :  0.23786E+00 0.12496E+01
   Friction velocity        uet   :  0.14228E-01 0.73033E-01
   Friction velocity        uk    :  0.17293E-01 0.38587E-01
   Dimensionless distance   yplus :  0.42547E+03 0.94504E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66060E+01      59   0.12702E-02   0.21643E-01 
c  VelocityX    0.46301E+04      12   0.68421E-02   0.37122E-03 
c  VelocityY    0.46301E+04      12   0.68421E-02   0.27128E-04 
c  VelocityZ    0.46301E+04      12   0.68421E-02   0.36807E-04 
c  TurbEner     0.59754E+01      13   0.68251E-04   0.93589E-09 
c  Dissip       0.13202E+01      15   0.56861E-03   0.81787E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.39           54551           26777           27271
v  Velocity[x]            0.29278          2.1473         0.90807         0.90984
v  Velocity[y]           -0.36699         0.70915      0.00055255      0.00032945
v  Velocity[z]           -0.42263         0.50471      -0.0012585      -0.0013771
v  TurbEner            0.00099892        0.014636       0.0032849       0.0033447
v  Dissip              9.2087e-05         0.02678      0.00044888      0.00038857
v  TurbVisc               0.16347          11.332          4.7135          5.2746
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              985:        0.89687E-01

===============================================================


 INSTANT    0.986000000E+03   TIME STEP NUMBER             986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001937E+04
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 :  0.23761E+00 0.13235E+01
   Friction velocity        uet   :  0.14213E-01 0.78869E-01
   Friction velocity        uk    :  0.17311E-01 0.38598E-01
   Dimensionless distance   yplus :  0.42505E+03 0.94440E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.60256E+01      55   0.15733E-02   0.19762E-01 
c  VelocityX    0.46301E+04      12   0.70178E-02   0.41694E-03 
c  VelocityY    0.46301E+04      12   0.70178E-02   0.34598E-04 
c  VelocityZ    0.46301E+04      12   0.70178E-02   0.45849E-04 
c  TurbEner     0.59768E+01      13   0.11696E-03   0.17598E-08 
c  Dissip       0.13448E+01      17   0.20116E-02   0.53012E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.57           54543           26778           27272
v  Velocity[x]            0.29275          1.9987         0.90808         0.90986
v  Velocity[y]           -0.38243         0.70078      0.00056129      0.00034133
v  Velocity[z]           -0.41874         0.51181      -0.0012562      -0.0013756
v  TurbEner             0.0010002        0.015221       0.0032855       0.0033451
v  Dissip              9.2081e-05        0.028274      0.00044929      0.00038886
v  TurbVisc               0.16347          11.322          4.7136          5.2747
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              986:        0.89712E-01

===============================================================


 INSTANT    0.987000000E+03   TIME STEP NUMBER             987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998141E+04
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 :  0.23755E+00 0.12515E+01
   Friction velocity        uet   :  0.14208E-01 0.72792E-01
   Friction velocity        uk    :  0.17322E-01 0.38620E-01
   Dimensionless distance   yplus :  0.42566E+03 0.94373E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66758E+01      62   0.15415E-02   0.21897E-01 
c  VelocityX    0.46301E+04      12   0.67791E-02   0.43043E-03 
c  VelocityY    0.46301E+04      12   0.67791E-02   0.29232E-04 
c  VelocityZ    0.46301E+04      12   0.67791E-02   0.10923E-03 
c  TurbEner     0.59763E+01      14   0.11950E-03   0.21720E-08 
c  Dissip       0.13266E+01      16   0.15895E-02   0.37009E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.77           54518           26777           27272
v  Velocity[x]            0.29256          2.0812         0.90808         0.90985
v  Velocity[y]           -0.36696         0.70724      0.00056913      0.00034636
v  Velocity[z]           -0.42034          0.5057      -0.0012413      -0.0013627
v  TurbEner            0.00099914         0.01469       0.0032858       0.0033453
v  Dissip              9.2073e-05         0.02723      0.00044933      0.00038889
v  TurbVisc               0.16397          11.357          4.7138          5.2749
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              987:        0.90198E-01

===============================================================


 INSTANT    0.988000000E+03   TIME STEP NUMBER             988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001744E+04
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 :  0.23765E+00 0.13257E+01
   Friction velocity        uet   :  0.14214E-01 0.79001E-01
   Friction velocity        uk    :  0.17313E-01 0.38639E-01
   Dimensionless distance   yplus :  0.42573E+03 0.94331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55329E+01      53   0.11951E-02   0.18150E-01 
c  VelocityX    0.46302E+04      12   0.67406E-02   0.33481E-03 
c  VelocityY    0.46302E+04      12   0.67406E-02   0.27561E-04 
c  VelocityZ    0.46302E+04      12   0.67406E-02   0.46298E-04 
c  TurbEner     0.59757E+01      13   0.75624E-04   0.12034E-08 
c  Dissip       0.13339E+01      15   0.59786E-03   0.86704E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.94           54526           26778           27272
v  Velocity[x]            0.29293          2.1328         0.90806         0.90983
v  Velocity[y]           -0.38279         0.70087       0.0005568      0.00033478
v  Velocity[z]           -0.42008         0.51062      -0.0012485      -0.0013683
v  TurbEner             0.0010026        0.014613        0.003286       0.0033454
v  Dissip              9.2091e-05        0.027096       0.0004495      0.00038898
v  TurbVisc               0.16409           11.33           4.714           5.275
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              988:        0.88915E-01

===============================================================


 INSTANT    0.989000000E+03   TIME STEP NUMBER             989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000207E+04
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 :  0.23823E+00 0.12252E+01
   Friction velocity        uet   :  0.14249E-01 0.72321E-01
   Friction velocity        uk    :  0.17343E-01 0.38635E-01
   Dimensionless distance   yplus :  0.42545E+03 0.94254E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.63599E+01      52   0.12986E-02   0.20846E-01 
c  VelocityX    0.46303E+04      12   0.68184E-02   0.35692E-03 
c  VelocityY    0.46303E+04      12   0.68184E-02   0.23564E-04 
c  VelocityZ    0.46303E+04      12   0.68184E-02   0.31171E-04 
c  TurbEner     0.59767E+01      13   0.73332E-04   0.84626E-09 
c  Dissip       0.13581E+01      15   0.83991E-03   0.15205E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.81           54536           26777           27271
v  Velocity[x]             0.2928          2.1733         0.90805         0.90983
v  Velocity[y]           -0.36733         0.70926      0.00056011      0.00033555
v  Velocity[z]           -0.42091         0.50439      -0.0012443      -0.0013638
v  TurbEner             0.0010075        0.014753       0.0032863       0.0033455
v  Dissip              9.2035e-05          0.0275       0.0004498      0.00038917
v  TurbVisc               0.16415          11.331          4.7141          5.2751
v  total_pressure           83083      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              989:        0.88859E-01

===============================================================


 INSTANT    0.990000000E+03   TIME STEP NUMBER             990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001411E+04
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 :  0.23768E+00 0.13255E+01
   Friction velocity        uet   :  0.14215E-01 0.78999E-01
   Friction velocity        uk    :  0.17385E-01 0.38601E-01
   Dimensionless distance   yplus :  0.42684E+03 0.94301E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.59406E+01      60   0.12314E-02   0.19491E-01 
c  VelocityX    0.46302E+04      12   0.66935E-02   0.35019E-03 
c  VelocityY    0.46302E+04      12   0.66935E-02   0.42424E-04 
c  VelocityZ    0.46302E+04      12   0.66935E-02   0.29206E-04 
c  TurbEner     0.59773E+01      13   0.12427E-03   0.15726E-08 
c  Dissip       0.13782E+01      16   0.19910E-02   0.46843E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -167.77           54545           26779           27273
v  Velocity[x]            0.29259          2.0033         0.90806         0.90983
v  Velocity[y]           -0.38225         0.69905      0.00055715      0.00033468
v  Velocity[z]           -0.42176         0.51187      -0.0012504      -0.0013729
v  TurbEner             0.0010077        0.015379       0.0032866       0.0033457
v  Dissip              9.2059e-05        0.029052      0.00045016      0.00038942
v  TurbVisc               0.16508          11.361          4.7143          5.2752
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              990:        0.90311E-01

===============================================================


 INSTANT    0.991000000E+03   TIME STEP NUMBER             991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399997352E+04
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 :  0.23772E+00 0.12379E+01
   Friction velocity        uet   :  0.14218E-01 0.72523E-01
   Friction velocity        uk    :  0.17387E-01 0.38435E-01
   Dimensionless distance   yplus :  0.42706E+03 0.94346E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57690E+01      54   0.12837E-02   0.18914E-01 
c  VelocityX    0.46302E+04      12   0.68992E-02   0.26231E-03 
c  VelocityY    0.46302E+04      12   0.68992E-02   0.20120E-04 
c  VelocityZ    0.46302E+04      12   0.68992E-02   0.48777E-04 
c  TurbEner     0.59766E+01      13   0.11299E-03   0.16057E-08 
c  Dissip       0.13553E+01      16   0.16219E-02   0.43179E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.24           54553           26778           27273
v  Velocity[x]            0.29283          2.0829         0.90805         0.90982
v  Velocity[y]           -0.36615         0.70567      0.00056083      0.00033535
v  Velocity[z]           -0.42149         0.50653      -0.0012523      -0.0013755
v  TurbEner             0.0010147         0.01486       0.0032866       0.0033458
v  Dissip              9.2056e-05        0.028066       0.0004501      0.00038938
v  TurbVisc               0.16525          11.343          4.7143          5.2753
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              991:        0.89224E-01

===============================================================


 INSTANT    0.992000000E+03   TIME STEP NUMBER             992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999210E+04
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 :  0.23791E+00 0.13251E+01
   Friction velocity        uet   :  0.14229E-01 0.78968E-01
   Friction velocity        uk    :  0.17448E-01 0.38456E-01
   Dimensionless distance   yplus :  0.42771E+03 0.94383E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62615E+01      59   0.15783E-02   0.20527E-01 
c  VelocityX    0.46302E+04      12   0.68176E-02   0.34813E-03 
c  VelocityY    0.46302E+04      12   0.68176E-02   0.29658E-04 
c  VelocityZ    0.46302E+04      12   0.68176E-02   0.44724E-04 
c  TurbEner     0.59773E+01      12   0.59697E-04   0.61679E-09 
c  Dissip       0.13689E+01      14   0.38207E-03   0.36887E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -166.45           54545           26779           27273
v  Velocity[x]              0.293          2.1353         0.90809         0.90987
v  Velocity[y]           -0.38235         0.69905      0.00055473      0.00033268
v  Velocity[z]           -0.42022         0.51101      -0.0012503      -0.0013713
v  TurbEner               0.00102        0.014779        0.003287       0.0033461
v  Dissip              9.2059e-05        0.028008      0.00045028       0.0003895
v  TurbVisc               0.16577          11.339          4.7145          5.2754
v  total_pressure           83077      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              992:        0.89656E-01

===============================================================


 INSTANT    0.993000000E+03   TIME STEP NUMBER             993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399998430E+04
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 :  0.23736E+00 0.12133E+01
   Friction velocity        uet   :  0.14196E-01 0.72314E-01
   Friction velocity        uk    :  0.17493E-01 0.38522E-01
   Dimensionless distance   yplus :  0.42919E+03 0.94476E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65843E+01      60   0.15448E-02   0.21596E-01 
c  VelocityX    0.46303E+04      13   0.71267E-02   0.37731E-03 
c  VelocityY    0.46303E+04      13   0.71267E-02   0.38615E-04 
c  VelocityZ    0.46303E+04      13   0.71267E-02   0.10110E-03 
c  TurbEner     0.59783E+01      13   0.78207E-04   0.12076E-08 
c  Dissip       0.13947E+01      16   0.90221E-03   0.19124E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.19           54519           26778           27273
v  Velocity[x]            0.29255          2.1805         0.90807         0.90984
v  Velocity[y]           -0.36774         0.70805      0.00056854      0.00034479
v  Velocity[z]           -0.41968         0.50413      -0.0012356      -0.0013575
v  TurbEner             0.0010221        0.014877       0.0032872       0.0033462
v  Dissip              9.2076e-05        0.028383      0.00045059      0.00038971
v  TurbVisc               0.16669          11.318          4.7147          5.2756
v  total_pressure           83084      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              993:        0.90446E-01

===============================================================


 INSTANT    0.994000000E+03   TIME STEP NUMBER             994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002352E+04
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 :  0.23794E+00 0.13241E+01
   Friction velocity        uet   :  0.14231E-01 0.78921E-01
   Friction velocity        uk    :  0.17511E-01 0.38573E-01
   Dimensionless distance   yplus :  0.43001E+03 0.94520E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61212E+01      56   0.14993E-02   0.20086E-01 
c  VelocityX    0.46302E+04      12   0.70351E-02   0.42928E-03 
c  VelocityY    0.46302E+04      12   0.70351E-02   0.29212E-04 
c  VelocityZ    0.46302E+04      12   0.70351E-02   0.39849E-04 
c  TurbEner     0.59782E+01      13   0.12046E-03   0.15912E-08 
c  Dissip       0.14162E+01      16   0.21874E-02   0.57233E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.26           54529           26779           27274
v  Velocity[x]            0.29269          2.0187         0.90806         0.90984
v  Velocity[y]           -0.38253         0.69871      0.00056191      0.00033688
v  Velocity[z]           -0.42139         0.51174      -0.0012463      -0.0013693
v  TurbEner             0.0010277        0.015496       0.0032874       0.0033464
v  Dissip               9.206e-05        0.030092      0.00045093      0.00038994
v  TurbVisc               0.16712          11.326          4.7147          5.2757
v  total_pressure           83077      1.5658e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              994:        0.89825E-01

===============================================================


 INSTANT    0.995000000E+03   TIME STEP NUMBER             995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999141E+04
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 :  0.23797E+00 0.12211E+01
   Friction velocity        uet   :  0.14232E-01 0.72497E-01
   Friction velocity        uk    :  0.17559E-01 0.38569E-01
   Dimensionless distance   yplus :  0.43028E+03 0.94565E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.56447E+01      58   0.13203E-02   0.18504E-01 
c  VelocityX    0.46302E+04      12   0.61927E-02   0.32849E-03 
c  VelocityY    0.46302E+04      12   0.61927E-02   0.24874E-04 
c  VelocityZ    0.46302E+04      12   0.61927E-02   0.48794E-04 
c  TurbEner     0.59770E+01      14   0.12365E-03   0.19821E-08 
c  Dissip       0.13958E+01      16   0.16185E-02   0.42915E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -174.83           54536           26778           27272
v  Velocity[x]            0.29306          2.0887         0.90804         0.90981
v  Velocity[y]           -0.36656         0.70536      0.00056553      0.00033777
v  Velocity[z]           -0.42135         0.50596      -0.0012471      -0.0013689
v  TurbEner             0.0010337        0.014951       0.0032873       0.0033463
v  Dissip              9.2037e-05          0.0291      0.00045085      0.00038988
v  TurbVisc               0.16738          11.362          4.7148          5.2758
v  total_pressure           83082      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              995:        0.90209E-01

===============================================================


 INSTANT    0.996000000E+03   TIME STEP NUMBER             996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400002552E+04
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 :  0.23765E+00 0.13251E+01
   Friction velocity        uet   :  0.14213E-01 0.78976E-01
   Friction velocity        uk    :  0.17610E-01 0.38570E-01
   Dimensionless distance   yplus :  0.43207E+03 0.94647E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53851E+01      53   0.12507E-02   0.17671E-01 
c  VelocityX    0.46302E+04      12   0.67003E-02   0.28333E-03 
c  VelocityY    0.46302E+04      12   0.67003E-02   0.22405E-04 
c  VelocityZ    0.46302E+04      12   0.67003E-02   0.47989E-04 
c  TurbEner     0.59773E+01      12   0.64824E-04   0.55999E-09 
c  Dissip       0.14048E+01      14   0.43011E-03   0.39331E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.81           54545           26778           27272
v  Velocity[x]            0.29262           2.139         0.90806         0.90984
v  Velocity[y]           -0.38226         0.69912      0.00055493      0.00033085
v  Velocity[z]            -0.4213         0.51104      -0.0012551      -0.0013801
v  TurbEner              0.001033        0.014828       0.0032875       0.0033464
v  Dissip              9.2044e-05        0.028966      0.00045098      0.00038996
v  TurbVisc               0.16844          11.346          4.7149          5.2759
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              996:        0.89030E-01

===============================================================


 INSTANT    0.997000000E+03   TIME STEP NUMBER             997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000869E+04
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 :  0.23795E+00 0.12373E+01
   Friction velocity        uet   :  0.14231E-01 0.72297E-01
   Friction velocity        uk    :  0.17604E-01 0.38515E-01
   Dimensionless distance   yplus :  0.43226E+03 0.94651E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.74816E+01      65   0.14520E-02   0.24530E-01 
c  VelocityX    0.46303E+04      13   0.73880E-02   0.34314E-03 
c  VelocityY    0.46303E+04      13   0.73880E-02   0.47989E-04 
c  VelocityZ    0.46303E+04      13   0.73880E-02   0.87949E-04 
c  TurbEner     0.59784E+01      12   0.65313E-04   0.68394E-09 
c  Dissip       0.14333E+01      15   0.82622E-03   0.16198E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -177.21           54552           26777           27271
v  Velocity[x]            0.29276          2.1855         0.90805         0.90981
v  Velocity[y]           -0.36689         0.70754      0.00057205      0.00034713
v  Velocity[z]           -0.42139          0.5048      -0.0012432      -0.0013672
v  TurbEner             0.0010383        0.014921       0.0032875       0.0033465
v  Dissip              9.2023e-05        0.029269       0.0004512      0.00039011
v  TurbVisc                0.1685          11.344           4.715           5.276
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              997:        0.92150E-01

===============================================================


 INSTANT    0.998000000E+03   TIME STEP NUMBER             998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400001706E+04
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 :  0.23779E+00 0.13248E+01
   Friction velocity        uet   :  0.14222E-01 0.78965E-01
   Friction velocity        uk    :  0.17649E-01 0.38591E-01
   Dimensionless distance   yplus :  0.43260E+03 0.94683E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.72595E+01      61   0.16805E-02   0.23787E-01 
c  VelocityX    0.46301E+04      12   0.76584E-02   0.44349E-03 
c  VelocityY    0.46301E+04      12   0.76584E-02   0.65855E-04 
c  VelocityZ    0.46301E+04      12   0.76584E-02   0.48286E-04 
c  TurbEner     0.59789E+01      13   0.13026E-03   0.19023E-08 
c  Dissip       0.14438E+01      16   0.20327E-02   0.48944E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -169.77           54543           26777           27271
v  Velocity[x]            0.29292          2.0047         0.90808         0.90985
v  Velocity[y]           -0.38235         0.69868      0.00056012      0.00033895
v  Velocity[z]           -0.41902         0.51179      -0.0012469      -0.0013698
v  TurbEner             0.0010407        0.015587       0.0032879       0.0033467
v  Dissip              9.2045e-05        0.030849      0.00045156      0.00039037
v  TurbVisc               0.16879          11.377          4.7151          5.2761
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              998:        0.91010E-01

===============================================================


 INSTANT    0.999000000E+03   TIME STEP NUMBER             999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.399999212E+04
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 :  0.23745E+00 0.12395E+01
   Friction velocity        uet   :  0.14201E-01 0.72503E-01
   Friction velocity        uk    :  0.17670E-01 0.38670E-01
   Dimensionless distance   yplus :  0.43356E+03 0.94637E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.69962E+01      59   0.15950E-02   0.22957E-01 
c  VelocityX    0.46303E+04      12   0.65621E-02   0.44671E-03 
c  VelocityY    0.46303E+04      12   0.65621E-02   0.38347E-04 
c  VelocityZ    0.46303E+04      12   0.65621E-02   0.33821E-04 
c  TurbEner     0.59785E+01      14   0.13443E-03   0.22523E-08 
c  Dissip       0.14204E+01      16   0.19045E-02   0.54314E-08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -176.95           54517           26777           27271
v  Velocity[x]            0.29245           2.098         0.90807         0.90984
v  Velocity[y]           -0.36685         0.70571      0.00056536      0.00034249
v  Velocity[z]           -0.42091         0.50575      -0.0012391      -0.0013592
v  TurbEner             0.0010403        0.014978       0.0032879       0.0033468
v  Dissip              9.2037e-05        0.029591      0.00045145       0.0003903
v  TurbVisc               0.16939          11.357          4.7152          5.2763
v  total_pressure           83081      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP              999:        0.89607E-01

===============================================================


 INSTANT    0.100000000E+04   TIME STEP NUMBER            1000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252        -0.400000000E+04
Smooth wall               5        2770         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         288         0.400000002E+04
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 :  0.23777E+00 0.13249E+01
   Friction velocity        uet   :  0.14221E-01 0.78967E-01
   Friction velocity        uk    :  0.17666E-01 0.38695E-01
   Dimensionless distance   yplus :  0.43390E+03 0.94575E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       2770
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration       1000, Physical time    0.10000E+04


   ** 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:    0.72981E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.65830E+01      57   0.14085E-02   0.21583E-01 
c  VelocityX    0.46302E+04      12   0.70512E-02   0.37160E-03 
c  VelocityY    0.46302E+04      12   0.70512E-02   0.35343E-04 
c  VelocityZ    0.46302E+04      12   0.70512E-02   0.41981E-04 
c  TurbEner     0.59782E+01      13   0.69214E-04   0.10794E-08 
c  Dissip       0.14308E+01      14   0.31012E-03   0.30489E-09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  Dissip  


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -168.29           54525           26778           27272
v  Velocity[x]            0.29279          2.1399         0.90806         0.90985
v  Velocity[y]           -0.38283         0.69887      0.00055269      0.00033084
v  Velocity[z]           -0.42213          0.5105       -0.001245      -0.0013688
v  TurbEner             0.0010433        0.014971       0.0032879       0.0033468
v  Dissip              9.2052e-05        0.029602      0.00045155      0.00039036
v  TurbVisc               0.16953          11.372          4.7153          5.2763
v  total_pressure           83076      1.5657e+05      1.1922e+05      1.1999e+05


 TIME FOR THE TIME STEP             1000:        0.10621E+00

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.13165E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:             94.852 s
  System CPU time:            0.208 s
  Total CPU time:           380.436 s

  Elapsed time:              95.504 s
  CPU / elapsed time          0.995

Memory use summary:

  Total memory used:                             952.633 MiB
                             local minimum:      237.582 MiB  (rank 2)
                             local maximum:      238.691 MiB  (rank 1)
  Theoretical instrumented dynamic memory:        26.849 MiB
                             local minimum:        6.354 MiB  (rank 2)
                             local maximum:        7.054 MiB  (rank 1)
